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  • Polymer and Materials Science  (148)
  • Aircraft Propulsion and Power  (38)
  • 42.75
  • Animals
  • 2005-2009
  • 1980-1984
  • 1950-1954
  • 1945-1949  (186)
  • 1948  (186)
Collection
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Years
  • 2005-2009
  • 1980-1984
  • 1950-1954
  • 1945-1949  (186)
Year
  • 1
    Publication Date: 2019-06-28
    Description: A theory has been developed for resetting the blade angles of an axial-flow compressor in order to improve the performance at speeds and flows other than the design and thus extend the useful operating range of the compressor. The theory is readily applicable to the resetting of both rotor and stator blades or to the resetting of only the stator blades and is based on adjustment of the blade angles to obtain lift coefficients at which the blades will operate efficiently. Calculations were made for resetting the stator blades of the NACA eight-stage axial-flow compressor for 75 percent of design speed and a series of load coefficients ranging from 0.28 to 0.70 with rotor blades left at the design setting. The NACA compressor was investigated with three different blade settings: (1) the design blade setting, (2) the stator blades reset for 75 percent of design speed and a load coefficient of 0.48, and (3) the stator blades reset for 75 percent of design speed and a load coefficient of 0.65.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-TR-915 , NACA-ACR-E6E02
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  • 2
    Publication Date: 2019-08-16
    Description: A wind tunnel investigation was conducted to determine the performance of a 4000-pound-thrust axial-flow turbojet engine with a high flow compressor. Pressure altitudes included 5000 to 40000 feet with ram pressure ratios from 1.00 to 1.82. Altitudes included 20000 to 40000 feet and ram pressure ratios from 1.09 to 1.75. A comparison is made between engine performance with high flow and low flow compressors.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8F09b
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  • 3
    Publication Date: 2019-08-16
    Description: A wind tunnel investigation was conducted to determine the performance of a turbine operating as an integral part of a turbojet engine. Data was obtained while the engine was running over full operable range of speeds at various altitudes and flight mach numbers, and with four nozzles of different outlet areas.A maximum turbine efficiency of 0.875 was obtained at altitude of 15 thousand feet, Mach number 0.53, and corrected turbine speed of 5900 rpm.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8A23
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  • 4
    Publication Date: 2019-08-16
    Description: Temperature and pressure distributions for an original and modified 3000 pound thrust axial flow turbojet engine were investigated. Data are included for a range of simulated altitudes from 5000 to 45000 feet, Mach numbers from 0.24 to 1.08, and corrected engine speeds from 10,550 to 13,359 rpm.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8C17
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  • 5
    Publication Date: 2019-07-11
    Description: This report presents the results of the tests of a power-plant installation to improve the circumferential pressure-recovery distribution at the face of the engine. An underslung "C" cowling was tested with two propellers with full cuffs and with a modification to one set of cuffs. Little improvement was obtained because the base sections of the cuffs were stalled. A set of guide vanes boosted the over-all pressures and helped the pressure recoveries for a few of the cylinders. Making the underslung cowling into a symmetrical "C" cowling evened the pressure distribution; however, no increases in front pressures were obtained. The pressures at the top cylinders remained low and the high pressures at the bottom cylinders were reduced. At higher powers and engine speeds, the symmetrical cowling appeared best from the standpoint of over-all cooling characteristics.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SL7L10
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  • 6
    Publication Date: 2019-07-11
    Description: An investigation was conducted in the Cleveland altitude wind tunnel to determine the operational characteristics of an axial flow-type turbojet engine with a 4000-pound-thrust rating over a range of pressure altitudes from 5,000 to 50,OOO feet, ram pressure ratios from 1.00 to 1.86, and temperatures from 60 deg to -50 deg F. The low-flow (standard) compressor with which the engine was originally equipped was replaced by a high-flow compressor for part of the investigation. The effects of altitude and airspeed on such operating characteristics as operating range, stability of combustion, acceleration, starting, operation of fuel-control systems, and bearing cooling were investigated. With the low-flow compressor, the engine could be operated at full speed without serious burner unbalance at altitudes up to 50,000 feet. Increasing the altitude and airspeed greatly reduced the operable speed range of the engine by raising the minimum operating speed of the engine. In several runs with the high-flow compressor the maximum engine speed was limited to less than 7600 rpm by combustion blow-out, high tail-pipe temperatures, and compressor stall. Acceleration of the engine was relatively slow and the time required for acceleration increased with altitude. At maximum engine speed a sudden reduction in jet-nozzle area resulted in an immediate increase in thrust. The engine started normally and easily below 20,000 feet with each configuration. The use of a high-voltage ignition system made possible starts at a pressure altitude of 40,000 feet; but on these starts the tail-pipe temperatures were very high, a great deal of fuel burned in and behind the tail-pipe, and acceleration was very slow. Operation of the engine was similar with both fuel regulators except that the modified fuel regulator restricted the fuel flow in such a manner that the acceleration above 6000 rpm was very slow. The bearings did not cool properly at high altitudes and high engine speeds with a low-flow compressor, and bearing cooling was even poorer with a high-flow compressor.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8F09a
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  • 7
    Publication Date: 2019-07-11
    Description: The effect of rotor-blade length, inlet angle, and shrouding was investigated with four different nozzles in a single-stage modification of the Mark 25 aerial-torpedo power plant. The results obtained with the five special rotor configurations are compared with those of the standard first-stage rotor with each nozzle. Each nozzle-rotor combination was operated at nominal pressure ratios of 8, 15 (design), and 20 over a range of speeds from 6000 rpm to the design speed of 18,000 rpm. Inlet temperature and pressure conditions of 1OOOo F and 95 pounds per square inch gage, respectively, were maintained constant for all runs.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE9G20
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  • 8
    Publication Date: 2019-07-11
    Description: Flow-metering devices used by the NACA and by the manufacturer of the J33 turbojet engine were calibrated together to determine whether an observed discrepancy in weight flow of approximately 4 percent for the two separate investigations might be due to the different devices used to meter air flow. A commercial adjustable orifice and a square-edge flat-plate orifice used by the NACA and a flow nozzle used by the manufacturer were calibrated against surveys across the throat of the nozzle. It was determined that over a range of weight flows from 18 to 45 pounds per second the average weight flows measured by the metering device used for the compressor test would be 0.70 percent lower than those measured by the metering device used in the engine tests and the probable variation about this mean would be +/- 0.39 percent. The very close agreement of the metering devices shows that the greater part of the discrepancy in weight flow is attributable to the effect of inlet pressure.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE8H03
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  • 9
    Publication Date: 2019-07-11
    Description: An investigation was conducted in the NACA Cleveland altitude wind tunnel to evaluate the performance characteristics of the X24C-4B turbojet engine over a range of simulated altitudes from 5000 to 45,000 feet,simulated flight Mach numbers from 0 to 1.08, and engine speeds from 4000 to 12,500 rpm. Performance data are presented to show graphically the effects of altitude at a flight Mach number of 0.25 and of flight Mach number at an altitude of 25,000 feet. The performance data are generalized to show the applicability of methods used to determine performance at any altitude from data obtained at a given altitude. A complete tabulation of performance data, as well as lubrication- and fuel- system data, is presented.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE7L26
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  • 10
    Publication Date: 2019-07-11
    Description: Investigations were made of the turbine from a Mark 25 torpedo to determine the performance of the unit with three different turbine nozzles at various axial nozzle-wheel clearances. Turbine efficiency with a reamed nondivergent nozzle that uses the axial clearance space for gas expansion was little affected by increasing the axial running clearance from 0.030 to 0.150 inch. Turbine efficiency with cast nozzles that expanded the gas inside the nozzle passage was found to be sensitive to increased axial nozzle-wheel clearance. A cast nozzle giving a turbine brake efficiency of 0.525 at an axial running clearance of 0.035 inch gave a brake efficiency of 0.475 when the clearance was increased to 0.095 inch for the same inlet-gas conditions and blade-jet speed ratio. If the basis for computing the isentropic power available to the turbine is the temperature inside the nozzle rather then the temperature in the inlet-gas pipe, an increase in turbine efficiency of about 0.01 is indicated.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE8B04
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  • 11
    Publication Date: 2019-07-12
    Description: At the request of the Air Material Command, Arm Air Forces, an investigation was conducted at the NACA Cleveland laboratory to determine the performance characteristics of the XJ-41-V turbojet-engine compressor. The complete compressor was mounted on a collecting chamber having an annular air-flow passage simulating the burner annulus of the engine and was driven by an electric motor. The compressor was extensively instrumented to determine the overall performance of the compressor, the characteristic performance of each of the compressor components, the state of the air stream in the simulated burner annulus, and the operation of the compressor bearings. An initial investigation at an equivalent compressor speed of 8000 rpm was made to determine the performance of the compressor and the collecting chamber and to determine the similarity of the air stream at the entrance to the simulated burner annulus. The mechanical performance of the compressor over a range of actual compressors speeds from 3300 to 8000 rpm is reported.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E7A17a
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  • 12
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    In:  CASI
    Publication Date: 2019-08-17
    Description: Measurements on three tubes with flow regulated by suction at the trainling edge of the tube are described. It was possible to vary the mass of air flowing through the tube over a large range. Such tubes could be used for shrouded propellers.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-TM-1191 , Zentrale fuer Wissenschaftliches Berichtswesen der Luftfahrtforschung des Generalluftzeugmeisters; 1945
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  • 13
    Publication Date: 2019-08-15
    Description: A preliminary investigation of an axial-flow gas turbine-propeller engine was conduxted. Performance data were obtained for engine speeds from 8000 to 13,000 rpm and altitudes from 5000 to 35,000 feet and compressor inlet ram pressure ratios from 1.00 to 1.17.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8F10
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  • 14
    Publication Date: 2019-08-15
    Description: A 19XB-1 combustor was operated under conditions simulating zero-ram operation of the 19XB-1 turbojet engine at various altitudes and engine speeds. The combustion efficiencies and the altitude operational limits were determined; data were also obtained on the character of the combustion, the pressure drop through the combustor, and the combustor-outlet temperature and velocity profiles. At altitudes about 10,000 feet below the operational limits, the flames were yellow and steady and the temperature rise through the combustor increased with fuel-air ratio throughout the range of fuel-air ratios investigated. At altitudes near the operational limits, the flames were blue and flickering and the combustor was sluggish in its response to changes in fuel flow. At these high altitudes, the temperature rise through the combustor increased very slowly as the fuel flow was increased and attained a maximum at a fuel-air ratio much leaner than the over-all stoichiometric; further increases in fuel flow resulted in decreased values of combustor temperature rise and increased resonance until a rich-limit blow-out occurred. The approximate operational ceiling of the engine as determined by the combustor, using AN-F-28, Amendment-3, fuel, was 30,400 feet at a simulated engine speed of 7500 rpm and increased as the engine speed was increased. At an engine speed of 16,000 rpm, the operational ceiling was approximately 48,000 feet. Throughout the range of simulated altitudes and engine speeds investigated, the combustion efficiency increased with increasing engine speed and with decreasing altitude. The combustion efficiency varied from over 99 percent at operating conditions simulating high engine speed and low altitude operation to less than 50 percent at conditions simulating operation at altitudes near the operational limits. The isothermal total pressure drop through the combustor was 1.82 times as great as the inlet dynamic pressure. As expected from theoretical considerations, a straight-line correlation was obtained when the ratio of the combustor total pressure drop to the combustor-inlet dynamic pressure was plotted as a function of the ratio of the combustor-inlet air density to the combustor-outlet gas density. The combustor-outlet temperature profiles were, in general, more uniform for runs in which the temperature rise was low and the combustion efficiency was high. Inspection of the combustor basket after 36 hours of operation showed very little deterioration and no appreciable carbon deposits.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8J29
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  • 15
    Publication Date: 2019-08-15
    Description: Operating characteristics of the 11-stage 4000-pound-thrust axial-flow turbojet engine were determined. A standard compressor and a compressor with the blade angles of the rotor and stator blades increased 5 degrees to obtain greater air flow, were investigated.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8F09c
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  • 16
    Publication Date: 2019-08-15
    Description: Combustion chamber performance properties of a 3000-pound-thrust axial-flow turbojet engine were determined. Data are presented for a range of simulated altitudes from 15,000 to 45,0000 feet and a range of Mach numbers from 0.23 to 1.05 for various modifications of the engine.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8B19
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  • 17
    Publication Date: 2019-07-11
    Description: An investigation was conducted in the NACA Cleveland altitude wind tunnel to determine the operational characteristics of the Westinghouse 19B-2, 19B-8, and 19XB-l jet-propulsion engines. The 19B engine is one af the earliest experimental Westinghouse axial flow engines. The 19XB-1 engine is an experimental prototype of the Westinghouse 15 series, having a rated thrust of 1400 pounds. Improvements in performance and operational characteristics have resulted in the 19XB-2B engine with a rated thrust of 1600 pounds. The operational characteristics were determined over a range of simulated altitudes from 5000 to 30,000 feet for the 19B engines and from 5000 to 35000 feet for the 19XB-l engine at airspeed from 20 to 380 miles per hour. The affects of altitude and airspeed on such operating characteristics as operating range, stability of combustion, starting, acceleration, and functioning of the fuel-control system are discussed. Damage to the engines that occurred during the investigation is also briefly discussed. The changes made in the combustion-chamber configuration to improve the operating we are described.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8J28-Pt-1
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  • 18
    Publication Date: 2019-07-11
    Description: A theoretical investigation has been made of various methods of thrust augmentation for turbojet engines. The method investigated were tail-pipe burning, water injection at the compressor inlet, a combination of tail-pipe burning and water injection, bleedoff in conjunction with water injection at the compressor inlet, and rocket assist. The effect of ratio of augmented-to-normal total liquid consumption, flight conditions, and design compressor pressure ratio on the augmentation produced by each method were determined. A comparison was also made for a given time of operation of the weight of an augmented engine plus fuel and additional liquids to the weight of a standard engine plus fuel producing the same thrust.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8H11
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  • 19
    Publication Date: 2019-07-11
    Description: The Allison model 400-C6 compressor was operated at an inlet pressure of 12 inches of mercury absolute ana ambient inlet temperature at equivalent impeller speeds of 6000, 7000, and 8500 rpm. Additional runs at an equivalent speed of 7000 rpm and ambient inlet temperature were made at inlet pressures from 7 to 22 inches of mercury absolute. The results of this investigation are compared with those of the 533-A-23 compressors. For the speeds investigated, the Allison model 400-C6 compressor had a maximum adiabatic temperature-rise efficiency of 0.768 at an equivalent speed of 7000 rpm; the corresponding equivalent weight flow was 45.0 pounds per second and the pressure ratio was 1.83. At an equivalent impeller speed of 8500 rpm, the maximum equivalent weight flow was 61.6 pounds per second and the peak pressure ratio of 2.38 occurred at an equivalent weight flow of 52.2 pounds per 1 second and an adiabatic temperature-rise efficiency of 0.714. At an equivalent speed of 7000 rpm, increasing the compressor- inlet pressure increased the maximum equivalent weight flow and the pressure ratio.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE8L15
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  • 20
    Publication Date: 2019-07-11
    Description: The production-model 333-A-23 turbojet-engine compressor with a 17-blade impeller was operated at ambient and 0 F inlet temperatures and at inlet pressures of 14 and 5 inches mercury absolute for equivalent impeller speeds from 6000 to 12,750 rpm. The results of this investigation are compared with those of the 533-A-21 compressor. At the design equivalent speed of 11,750 rpm the maximum pressure ratio was 4.39. This occurred at the surge point at which the equivalent weight flow was 80.8 pounds per second, ana the adiabatic temperature-rise efficiency was 0.757. The maximum flow at the design equivalent speed was 88.0 pounds per second. The maximum adiabatic temperature-rise efficiency of 0.799 was obtained at an equivalent speed of 10,000 rpm, and equivalent weight flow of 62.9 pounds per second, and a pressure ratio of 3.20. At the maximum equivalent speed investigated (12,750 rpm), a peak pressure ratio of 4.90 was attained at an equivalent weight flow of 85.4 pounds per second and an efficiency of 0.680.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE8F15-Pt-1
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  • 21
    Publication Date: 2019-07-11
    Description: In an investigation of the J-33-A-21 and the J-33-A-23 compressors with and without water injection, it was discovered that the compressors reacted differently to water injection although they were physically similar. An analysis of the effect of water injection on compressor performance and the consequent effect on matching of the compressor and turbine components in the turbojet engine was made. The analysis of component matching is based on a turbine flow function defined as the product of the equivalent weight flow and the reciprocal of the compressor pressure ratio.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE8A19
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  • 22
    Publication Date: 2019-07-11
    Description: An investigation has been conducted in the NACA Cleveland altitude wind tunnel to evaluate the performance and windmilling drag characteristics of an original and a modified turbojet engine of the same type. Data have been obtained at simulated altitudes from 5000 to 45,000 feet, simulated flight Mach numbers from 0.09 to 1.08, and engine speeds from 4000 to 12,500 rpm. Engine performance data are presented for both engines to show the effects of altitude at a flight Mach number of 0.25 and of flight Mach number at an altitude of 25,000 feet. Performance of the original and modified engines is compared for a range of simulated flight conditions. The performance data are generalized to show the applicability of methods used to estimate performance at any altitude from data obtained at a given altitude. Engine-windmilling-speed and windmilling-drag data are presented for a range of simulated flight conditions.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8B26 , Rept-928
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  • 23
    Publication Date: 2019-07-11
    Description: An investigation was conducted in an altitude test chamber to determine the effects of inlet airflow distortion on the compressor steady-state and surge characteristics of a high-pressure ratio, axial-flow turbojet engine. Circumferential-type inlet flow distortions were investigated, which covered a range of distortion sector angles from 20 deg to 168 deg and distortion levels up to 22 percent. The presence of inlet airflow distortions at the compressor face resulted in a substantial increase in the local pressure ratio in the distorted region, primarily for the inlet stages. The local pressure ratio in the distorted region for the inlet stages increased as either the distortion sector angle decreased or the percent distortion increased. The average compressor-surge pressure ratio was much more sensitive to inlet airflow distortions at lower engine speeds than at engine speeds near rated. Hence, compressor-surge margin reduction due to inlet airflow distortion was quite severe at the lower engine speeds. Although the average compressor-surge pressure ratio was generally reduced with inlet flow distortion, local pressure ratios across the distorted sector of the compressor were obtained during surge and were significantly greater than the normal compressor-surge pressure ratio. This was a result of increased loading of the inlet stages in the distorted region.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E57L12
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  • 24
    Publication Date: 2019-07-11
    Description: An altitude-test-chamber investigation was conducted to determine the operational characteristics and altitude blow-out limits of a Solar afterburner in a 24C engine. At rated engine speed and maximum permissible turbine-discharge temperature, the altitude limit as determined by combustion blow-out occurred as a band of unstable operation of about 8000 feet altitude in width with maximum altitude limits from 32,000 feet at a Mach number of 0.3 to about 42,000 feet at a Mach number of 1.0. The maximum fuel-air ratio of the afterburner, as limited by maximum permissible turbine-discharge gas temperatures at rated engine speed, varied between 0.0295 and 0.0380 over a range of flight Mach numbers from 0.25 to 1.0 and at altitudes of 20,000 and 30,000 feet. Over this range of operating conditions, the fuel-air ratio at which lean blow-out occurred was from 10 to 19 percent below these maximum fuel-air ratios. Combustion was very smooth and uniform during operation; however, ignition of the burner was very difficult throughout the investigation. A failure of the flame holder after 12 hours and 15 minutes of afterburner operation resulted in termination of the investigation.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE8G02
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  • 25
    Publication Date: 2019-07-11
    Description: With the further development of axial blowers into highly loaded flow machines, the influence of the diameter ratio upon air output and efficiency gains in significance. Clarification of this matter is important for single-stage axial compressors, and is of still greater importance for multistage ones, and particularly for aircraft power plants. Tests with a single-stage axial blower gave a decrease in the attainable maximum pressure coefficient and optimum efficiency as the diameter ratio increased. The decrease must be ascribed chiefly to the guide surface of the hub and housing between the blades increasing with the diameter ratio.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-TM-1125
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  • 26
    Publication Date: 2019-07-11
    Description: As part of an investigation af the application of nuclear energy to various types of power plants for aircraft, calculations have been made to determine the effect of several operating conditions on the performance of condensers for mercury-turbine power plants. The analysis covered 8 range of turbine-outlet pressures from 1 to 200 pounds per square inch absolute, turbine-inlet pressures from 300 to 700 pounds per square inch absolute,and a range of condenser cooling-air pressure drops, airplane flight speeds, and altitudes. The maximum load-carrying capacity (available for the nuclear reactor, working fluid, and cargo) of a mercury-turbine powered aircraft would be about half the gross weight of the airplane at a flight speed of 509 miles per hour and an altitude of 30,000 feet. This maximum is obtained with specific condenser frontal areas of 0.0063 square foot per net thrust horsepower with the condenser in a nacelle and 0.0060 square foot per net thrust horsepower with the condenser submerged in the wings (no external condenser drag) for a turbine-inlet pressure of 500 pounds per square inch absolute, a turbine-outlet pressure of 10 pounds per square inch absolute, and 8 turbine-inlet temperature of 1600 F.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8C23 , Rept-952
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  • 27
    Publication Date: 2019-07-11
    Description: The J33-A-23 compressor with a 34-blade impeller was operated at ambient inlet temperature and an inlet pressure of 14 inches mercury absolute over a range of equivalent impeller speeds from 6000 to 11,750 rpm. Additional runs at equivalent speeds of 7,000, 10,000, and 11,750 rpm and ambient inlet temperature were made at inlet pressures of 5 and 10 inches mercury absolute. The results of this investigation are compared with those of the J33-A-23 compressor with a 17-blade impeller. At the design equivalent speed of 11,750 rpm the 533-A-23 compressor with a 34-blade impeller had a peak pressure ratio of 4.49 at an equivalent weight flow of 82.4 pounds per second and an adiabatic temperature-rise efficiency of 0.740. The maximum equivalent flow at design speed was 91.8 pounds per second. The peak efficiency at design speed (0.757) occurred at an equivalent weight flow of 85.5 pounds per second. The maximum adiabatic temperature- rise efficiency of 0.773 was obtained at an equivalent impeller speed of 10,000 rpm, an equivalent weight flow of 65.8 pounds per second, and a pressure ratio of 3.27. At equivalent impeller speeds of.l0,000 and 11,75O rpm a decrease in inlet pressure resulted in a decrease in maximum equivalent weight flow, peak pressure ratio, and peak adiabatic temperature- rise efficiency.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE8H13
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  • 28
    Publication Date: 2019-07-12
    Description: An investigation of the XJ-41-V turbojet-engine compressor was conducted to determine the performance of the compressor and to obtain fundamental information on the aerodynamic problems associated with large centrifugal-type compressors. The results of the research conducted on the original compressor indicated the compressor would not meet the desired engine-design air-flow requirements because of an air-flow restriction in the vaned collector. The compressor air-flow choking point occurred near the entrance to the vaned-collector passage and was instigated by a poor mass-flow distribution at the vane entrance and from relatively large negative angles of attack of the air stream along the entrance edges of the vanes at the outer passage wall and large positive angles of attack at the inner passage wall. As a result of the analysis, a design change of the vaned collector entrance is recommended for improving the maximum flow capacity of the compressor.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE7L12
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  • 29
    Publication Date: 2019-07-12
    Description: The performance of an annular combustion chamber from a 24C turbojet engine was investigated over a range of simulated altitudes from 20,000 to 55,000 feet and corrected engine rotor speeds from 6000 to 13,000 rpm at a simulated ram-pressure ratio of 1.04. The purpose of the investigation was to determine the effects on the altitude operational limits, combustor-outlet gas temperature distribution, combustion efficiencies, and combustor inlet-to-outlet total-pressure drops of two changes in the 24C-4B basket air-passage arrangements that were designed to improve combustor-outlet temperature distribution. These changes were: (a) replacement of the downstream secondary air holes with large rectangular slots further upstream (rectangular-slot basket), and (b) enlargement of anticoking holes in the rectangular-slot basket (modified rectangular-slot basket). The results indicate that improved outlet-gas temperature distribution of each succeeding combustor basket investigated was attained at a sacrifice in the altitude limit of operation. The altitude limits of operation of the combustor with the original basket ranged from 34,000 feet at a corrected engine speed of 6000 rpm to a maximum of 52,000 feet at 12 ' 500 rpm. The altitude limits of the rectangular-slot basket were about 2000 feet lower throughout the engine speed range than those of the original basket. The altitude limits of the combustor with the modified rectangular-slot basket were about equivalent to those of the other baskets in the corrected-engine-speed range from 12,000 to 12,500 rpm but were about 10,000 feet lower than those of the original basket in the corrected-engine-speed range from 6000 to 9000 rpm. For the same inlet-air conditions, the combustion efficiencies were highest for the original basket and progressively lower for each of the other two baskets. The combustor inlet-to-outlet pressure drops of all three combustor baskets at the same operating conditions were within +/- 10 percent of the pressure drop of the original basket.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE8G13
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  • 30
    Publication Date: 2019-07-12
    Description: Compressor operation at low air flows for a given speed is limited by unstable flow conditions, commonly called surge. An investigation of surge in centrifugal compressors (reference 1) showed that the pulsation of pressures and velocities occurred when the slope of the compressor characteristic curve was positive and that the magnitude and frequency, as well as the incidence of surge, depended on the capacity and resistance of the total system. Although the theory presented in reference 1 is applicable to axial-floe compressors, little experimental information is available on the surge characteristics of the individual stages of axial-flow compressors, or on the variation of the surge characteristics with operating conditions. During the investigation to determine the performance of the X24C-2 compressor (references 2 and 3), instrumentation was added to study the surge characteristics and to determine the effect of speed and inlet pressure on the frequency, amplitude, and phase relation of the pressure pulsations behind each stage.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE8H06
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  • 31
    Publication Date: 2019-08-15
    Description: Compressor performance properties for two 11-stage compressors of 3000-pound-thrust axial-flow turbojet engines were determined. Data are presented for a range of simulated altitudes and a range of Mach numbers for various modifications of the engine.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8A26a
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  • 32
    Publication Date: 2019-08-15
    Description: Wind tunnel investigations were performed to determine the performance properties of an axial-flow gas turbine-propeller engine II. Windmilling characteristics were determined for a range of altitudes from 5000 to 35,000 feet, true airspeeds from 100 to 273 miles per hour, and propeller blade angles from 4 degrees to 46 degrees.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8F10a
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  • 33
    Publication Date: 2019-08-16
    Description: A simulated altitude performance of a 25 1/2-inch-diameter annular-type turbojet combustor was performed to determine the effect of the distribution of basket-hole area on the altitude operational limits of the engine as imposed by the combustor.Total pressure drop was recorded, as well as the effect of fuel-nozzle flow capacity,and fuel-nozzle spray angle for one basket configuration. General observations were made for all configurations regarding flames, extent of afterburning, and durability of the baskets.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8A02
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  • 34
    Publication Date: 2019-08-16
    Description: An investigation was conducted to evaluate the operational characteristics of a 3000 pound thrust axial flow turbojet engine over a range of simulated altitudes from 2000 to 50,000 feet and simulated flight Mach numbers from 0 to 1.04 throughout the operable range of engine speeds. Engine operating range, acceleration, deceleration, starting, altitude, and flight Mach number compensation of the fuel control system, and operation of the lubrication system at high and low ambient air temperatures were evaluated.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8B19a
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  • 35
    Publication Date: 2019-07-12
    Description: An investigation is being conducted to determine the altitude performance characteristics of the Nene II engine and its components. The present paper presents preliminary results obtained using a jet nozzle of 18.41 inches in diameter, giving an area equal to 96.4 percent of the area of the standard jet nozzle of this engine. The test results presented are for conditions simulating altitudes from seal level to 50,000 feet and ram-pressure ratios from 1.00 to 2.70. The ram pressure ratios correspond to flight Mach numbers between zero and 1.28.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8F14
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  • 36
    Publication Date: 2019-07-12
    Description: At the request of the Air Material Command, Army Air Forces, an investigation was conducted by the NACA Cleveland laboratory to determine the performance characteristics of the compressor of the XJ-41-V turbojet engine. This report is the second in a series presenting the compressor performance and analysis of flow conditions in the compressor. The static-pressure variation in the direction of flow through the compressor and the location and the cause of the maximum flow restriction at an equivalent speed of 8000 rpm are presented. After the initial runs were reported, the leading edges of the impeller blades and the diffuser surfaces were found to have been roughened by steel particles from a minor failure of auxiliary equipment. The leading edges of the impeller blades were refinished and all high spots resulting from scratches in the diffuser and the accessible parts of the vaned collector passages were removed. The initial overall performance and that obtained with the refinished blades are presented.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E7E05
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  • 37
    Publication Date: 2019-07-12
    Description: An extended analysis was made of the previously reported performance investigation of the original compressor from the XJ-41-v turbojet engine and a similar compressor revised a to obtain a 33-percent increase in the geometric passage area at the vaned-collector entrance. This analysis was based on the concept of the vaned-collector entrance as the throat section of a nozzle. Because of nonuniform air distribution at the vaned-collector entrance, approximately 90 percent of the available flow area was utilized in the original compressor and 94percent in the revised com$ressor. The increase in maximum weight flow obtained with the revised compressor was disproportionate to the increased effective critical throat area because. the air density at the revised vaned-collector entrance for maximum flow was lower than that obtained in the original compressor. This reduction in density resulted from the large pressure losses near the impeller inlet of the revised compressor, which is indicative of impending flow choking in the impeller, The.calculated maximum corrected weight-flow capacity of a compressor consisting of the revised vaneless diffuser and vaned collector with a theoretical impeller that combined peak impeller pressure ratio and peak impeller efficiency at the . maximum flow point would be 112 pounds per second for an equivalent impeller speed of 11,500 rpm;
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-SE8C12
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  • 38
    Publication Date: 2019-08-16
    Description: Performance properties and operational characteristics of an axial-flow gas turbine-propeller engine were determined. Data are presented for a range of simulated altitudes from 5,000 to 35,0000 feet, compressor inlet- ram pressure ratios from 1.00 to 1.17, and engine speeds from 8000 to 13,000 rpm.
    Keywords: Aircraft Propulsion and Power
    Type: NACA-RM-E8F10b
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  • 39
    Electronic Resource
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    Hoboken, NJ : Wiley-Blackwell
    Journal of Polymer Science 3 (1948), S. 32-38 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: Physical and mechanical properties of copolymers from dienes and acrylic nitrile have been studied. The gradual increase of density is an indication of the strong intermolecular forces exerted by nitrile groups. The mutual interaction of nitrile groups and methyl groups leads to a reduction of the mobility of flow units. This can be deduced from a relative comparison of hardness, elastic recovery, stress-strain properties, and brittle point of the three polymer-homologous series.
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  • 40
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: Recently published measurements of moisture sorption vs. relative humidity for a series of proteins have previously been analyzed in a way which permits calculation of the integral free energy of sorption for any final pressure of water vapor. The present paper is an extension of these calculations to additional proteins from the list reported by Bull; integral and differential free energies and integral and differential heats and entropies of sorption have been calculated as functions of the amounts of water sorbed onsilk, wool, egg albumin (unlyophilized and heat coagulated), salmine, collagen, gelatin and lactoglobulin (crystalline and lyophilized). All calculations are referred to saturated water vapor as the standard state. Some of the proteins show positive net differential entropies of sorption at low vapor pressures. It is postulated that the partial molal entropy of sorption is made up of two terms, a negative entropy of sorption proper and a positive entropy of solution. Partial rearrangements of the protein chains at the beginning of the sorption process would effectively be an incipient solution which would give rise to a positive partial molal entropy of sorption if the second term is greater than the first. This speculation has support in the fact that the differential entropy of salmine, which dissolves at a relative vapor pressure of about 0.7, begins to show positive values at a relative vapor pressure of 0.35.
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  • 41
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: Benzoyl, anisoyl, veratroyl, p-bromobenzoyl, p-phenylbenzoyl, p-benzoylbenzoyl, p-methylsulfonylbenzoyl, p(N,N-dimethylsulfonamido)-benzoyl and -naphthoyl disulfides are promoters of the emulsion copolymerization of butadiene and styrene, but exhibit little effect on the polymer properties. Furoyl, phenyl, p-chlorophenyl and p-bromophenyl disulfides are neither promoters nor modifiers.
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  • 42
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: Ten series of model filaments with increasing orientation and swelling degrees ranging between 16 and 1.2 were prepared from three viscoses containing 4, 6, and 10.5% cellulose. Their birefringence was measured and their x-ray diagrams taken and quantitatively evaluated in order to determine the over-all orientation of the iiber substance and that of the crystalline portion. It is shown that a general relation exists between the orientation of the crystallites and that of the entire fiber substance which is the same in all fibers stretched in the swollen state. Once the birefringence of a filament is known, the orientation factor of its crystallitee can be computed without taking an x-ray photograph. From the data further evidence can be derived to the effect that the orientation of the crystallitm cannot be accounted for by the theory of affined deformation.
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  • 43
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    Hoboken, NJ : Wiley-Blackwell
    Journal of Polymer Science 3 (1948), S. 157-166 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: In order to study further the effect of structure on monomer reactivities in copolymerization the copolymer composition as a function of initial monomer mixture composition has been determined for the following monomer pairs: vinyl acetate-vinyl chloride, ethyl methacrylate-vinylidene chloride, butyl methacrylate-vinylidene chloride, vinyl acetate-tetrachloroethylene, allyl chloride-vinylidene chloride, vinyl acetate-vinylidenechloride, methyl methacrylate-vinyl chloride, pentene-1-vinyl chloride, allyl chloride-vinyl acetate, methyl methacrylate-2,5-di-chlorostyrene, vinyl chloride-vinylidene chloride, and vinyl chloride-dioctyl maleate.
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  • 44
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    Journal of Polymer Science 3 (1948), S. 223-226 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: Crystalline chymotrypsin has been inactivated by ultraviolet light (2537 Å.) with a quantum yield of 0.0032 based upon loss of ability to act upon casein as a substrate. The possible significance of this datum in terms of the duo-specificity of chymotrypsin, the integrity of the molecule as a whole and the quantum efficiency of cleavage of —CONH— linkages is discussed. The ultraviolet light absorption spectrum of the pure enzyme has been determined.
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  • 45
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: Methods for the preparation of fiber-forming polymeric amides from ω-amino acids and The variation in melting points of the polymeric their amide-forming derivatives are described. The variation in melting points of the polymeric amides with increasing chain length of the recurring unit is discussed.
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  • 46
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    Hoboken, NJ : Wiley-Blackwell
    Journal of Polymer Science 3 (1948), S. 95-96 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Additional Material: 3 Ill.
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  • 47
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: A study has been made of the swelling characteristics of Styrene-divinylbenzene gels containing from 0.02 to 0.12% of the cross-linking agent. Variation in swelling of samples containing the same amount of divinylbenzene was shown to increase with decreasing divinylbenzene concentration. The influence of amount of cross-linking agent, type of solvent, and temperature, on equilibrium swelling is reported. By assuming that μg is 0.44 for polymer-toluene, values of μg for over 50 different solvents have been obtained. No values of μg below 0.42 were found. A correlation of swelling values and of μg values with cohesive energy densities of the solvents is presented. The polymer appears to have a cohesive energy density of 82 cal. per cc. Equilibrium swelling decreases slightly in toluene and methyl ethyl ketone but increases markedly in cyclohexane with rising temperature. Efforts to calculate gel constants from the temperature coefficient of swelling failed completely in the case of cyclohexane, and were only moderately successful with toluene. These temperature studies, and the cohesive energy density correlations both appear to indicate a lack of complete understanding about the physical significance of μ, and why it depends so markedly on concentration.
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  • 48
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    Journal of Polymer Science 3 (1948), S. 144-144 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
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  • 49
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    Hoboken, NJ : Wiley-Blackwell
    Journal of Polymer Science 3 (1948), S. 302-303 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
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  • 50
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    Hoboken, NJ : Wiley-Blackwell
    Journal of Polymer Science 3 (1948), S. 303-303 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
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  • 51
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    Hoboken, NJ : Wiley-Blackwell
    Journal of Polymer Science 3 (1948), S. 314-324 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The construction and operation of the osmotic balance has been described. Because of the damping effect of the cell immersed in the solvent the sensitivity of the balance is diminished. This can be avoided if a suitable weight is placed above the central knife-edge of the beam of the balance. A way to calculate the dimensions of a cell which gives the lowest possible temperature sensibility has been discussed. The disadvantage of a thick cell wall with respect to reference point adjustments has been pointed out. The measurements made with the balance have shown that osmotic pressures of the magnitude 0.011 ± 0.001 g./cm.2 can be measured. An example of the use of the balance has been given for three samples of nitrocellulose.
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  • 52
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    Journal of Polymer Science 3 (1948), S. 336-344 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Description / Table of Contents: The polymerization of indene catalyzed by oxygen at 30° and 40°C., has been studied. Oxygen is absorbed and a labile “oxypolymer” or “polyindene peroxyde” is formed and can be separated from normal polymer by precipitation.
    Notes: Es wird die Polymerisation von Inden unter Sauerstoffeinfluss bei 30 und 40°C. untersucht. Sauerstoff wird absorbiert unter Bildung eines labilen “Oxydpolymers” oder “Polyindenperoxyds,” das vom normalen Polymer mittels einer Fällungsreaktion getrennt werden kann.
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  • 53
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: A redox-activated emulsion polymerization system has been developed in which benzoyl peroxide, sorbose and ferrous ammonium sulfate constitute the oxidation reduction system. Very rapid rates of reaction were obtained which permitted the use of lower polymerization temperatures. Redox polymers made at 10°C. had higher molecular weights and superior physical properties compared to standard GR-S as well as to polymers prepared in the redox system at higher temperatures.
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  • 54
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The combination of a diazothio ether and a mercaptan in an emulsion copolymerization recipe of butadiene and styrene containing potassium ferricyanide as a “catalyst” has a very strong activating effect on the polymerization. p-Methoxyphenyl diazothio-(2-naphthyl) ether, designated as MDN, was found to be particularly suitable. In the present paper, ordinary household soap (S.F. flakes) and dehydrogenated rosin soaps of varying degrees of purity have been used as emulsifiers. By using various tertiary or primary mercaptans, polymers of any degree of modification were obtained. The recommended recipe at 40°C. gives about 80% conversion in 10 hours. The rate of conversion is greatly increased by adding to the recipe substances which have a strongly alkaline reaction in water, as sodium carbonate, trisodium phosphate, or sodium hydroxide. With such “alkaline” recipes attractive rates of conversion are obtained at around 0°C.
    Additional Material: 10 Ill.
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  • 55
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The German redox system of emulsion polymerization of butadiene and styrene has been found to be very sensitive to exact details of experimental procedure. Soap may be substituted for the alkanesulfonate used by the Germans; it is then unnecessary to add ferric laurate to the system.Careful investigation of the soap-emulsified mixture leads to the conclusion that 0.25 parts of benzoyl peroxide, 0.50 parts of ferrous sulfate heptahydrate, and 3.0 parts of sodium pyrophosphate decahydrate were the optimum concentrations of the essential ingredients for polymerization of an emulsion of 75 parts of butadiene and 25 parts of styrene in 200 parts of water and 5 parts of Procter and Gamble soap Flakes (S.F.) at 30°. At very low iron concentration the addition of a reducing agent as “booster” was beneficial; for this purpose sorbose can be replaced by fructose or, less satisfactorily, by a number of other reducing agents.
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  • 56
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    Journal of Polymer Science 3 (1948), S. 167-172 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: ε-Caprolactam is converted to ε-aminocaproic acid polymer by heating under pressure with water followed, by distillation of the water and heating at atmospheric pressure. The lactam is also polymerized directly to this polymer by a catalytic method in which sodiocaprolactam is the initiator.
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  • 57
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    Journal of Polymer Science 3 (1948), S. 216-222 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The emulsion polymerization of allyl acetate yields a polymer of the same average molecular weight as is obtained in bulk polymerization. The decomposition of potassimn persulfate is of the first order but is greatly accelerated by the presence of allyl acetate or of ethyl acetate. Three independent methods of analysis agree in indicating the presence of sulfate groups in 75% of the polymer molecules. It is concluded that the mechanisms of chain initiation and termination are analogous to those in the peroxide-induced bulk polymerization of allyl acetate. These facts do not serve to distinguish between different postulated loci reaction in emulsion polymerization.
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  • 58
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    Journal of Polymer Science 3 (1948), S. 227-230 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: An estimate of the magnitude of the interference effect in a coil-like molecule is made by calculating the nearest neighbor density w around a given link as a function of the total number of contributing chain units. It is shown, for instance, that in a chain consisting of several hundred units, the first fifteen contribute about 75 % of the total nearest neighbor density at distances below the length of a link. The plots presented indicate that after about the first twenty links, the rate of increase of nearest neighbor density begins to flatten off. It is also possible to derive the modification of the distribution function of chain ends in real chains for a given form of w.
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  • 59
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    Journal of Polymer Science 3 (1948), S. 297-301 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: Experimental results are reported for the copolymerization of cis- and trans-dichloroethylenes and trichloroethylene with vinyl acetate and styrene. Unsymmetrical as well as symmetrical 1,2 polysubstituted ethylenes exhibit extremely small rate constants for self-propagation, but are easily attacked by vinyl-type radicals such as that formed by vinyl acetate. The attack of such monomers by vinyl “growing chain” radicals is retarded by substitution on the attacked carbon atom, but is favored by substitution on the other carbon atom of the double bond.
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  • 60
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    Journal of Polymer Science 3 (1948), S. 302-302 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
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  • 61
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    Journal of Polymer Science 3 (1948), S. 518-524 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Description / Table of Contents: Polymeric indene prepared in the presence of oxygen can be separated into two fractions by precipitation with methanol. Polyindene is insoluble while the methanol-soluble portion can be precipitated from benzene by petroleum ether as a white powdery “polyindene peroxide.” Fractionation yielded samples with molecular weights from 300 to 3000. Bromine titration indicated that the lower molecular samples contained about one double bond per polymer molecule. The polymer gave qualitative tests for peroxide, but iodimetric titration of one sample gave only some 42.5% of the calculated active oxygen content.
    Notes: Polymeres Indol, das in Gegenwart von Sauerstoff dargestellt wurde, kann durch Fällen mit Methylalkohol in 2 Fraktionen getrennt werden. Polyindol ist unlöslich. Die methylalkohollösliche Fraktion kann aus Benzol mit Petroläther als ein weisses, pulveriges “Polyindolperoxyd” ausgefällt werden. Fraktionierung führte zu Substanzen mit Molekulargewichten zwischen 300 und 3000. Bromtitration deutete darauf hin, dass die niedrigmolekularen Proben ungefähr eine Doppelbindung pro Polymermolekül enthielten. Die qualitative Prüfung für Peroxyd war positiv, aber die jodometrische Titration einer Probe ergab nur 42.5% des berechneten aktiven Sauerstoffgehaltes.
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  • 62
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    Journal of Polymer Science 3 (1948), S. 525-534 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Description / Table of Contents: The reaction of indene with sulfur has been shown to give a polymer containing one atom of sulfur per indene unit. The refraction and absorption characteristics of the polymer have been reported. The kinetics of the reaction of sulfur, with and without added accelerators, have been investigated with the view to establishing the influence of the accelerators on the rate and the temperature coefficient.
    Notes: Es wird gezeigt, dass die Reaktion von Indol mit Schwefel zu einem Polymer führt, das ein Schwefelatom pro Indoleinheit enthält. Der Brechungsindex und das Absorptionsspektrum des Polymers werden mitgeteilt. Die Kinetik der Schwefelreaktion, mit und ohne Zusatz von Beschleunigern, wird untersucht um den Einfluss der Beschleuniger auf die Reaktiongeschwindigkeit und die Temperaturabhängigkeit der Reaktion festzustellen.
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  • 63
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    Journal of Polymer Science 3 (1948), S. 652-662 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: It has been demonstrated that the adhesion of high polymers to cellulose is a function of tack temperatures and dielectric constants, ∊, of the polymers and of dipole moments, μ, of polar groups. A plot of tack temperature versus mirror image force, μ1μ2/,of copolymers gives an area of adhesion bounded by a tack temperature of 100% and mirror image forces of 0.7 and 1.3 and opening toward lower tack temperatures. Outside of the area polymers do not adhere well to cellulose. By coating polymers on cellulose pretreated with Werner chromium complexes of acids bearing polar groups, it has been found that adhesion is a specific function of the polar groups within the polymer and on the modilied cellulose. Adhesion is strongest with approximately equal dipole moment substituents on the modified cellulose and in the copolymers.
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  • 64
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The peroxide-initiated polymerization of allyl methacrylate has been examined in the presence of certain additives. By the use of mercaptans and diisopropyl dixanthogen the extent of polymerization at the point where gelation occurs may be extended from about 6% to 20-30% polymerization. Examination of samples of polyallyl methacrylate, polymethyl methacrylate, and the copolymer of methyl methacrylate and allyl chloroacetate indicates that the postponement of gelation results largely from diminution of the molecular weight by the regulators. The effects of regulators on the composition of copolymers and the molecular weight of polymers, and the relation between molecular weight and extent of reaction at the gel point are discussed.
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  • 65
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The relaxation of stress in polyisobutylene whole polymer of different average molecular weights has been investigated over the temperature range 30-100°C., and at different elongations. The shape of the relaxation curve is independent of elongation in a range of low elongations; above this range there is a gradual change in curve shape with increasing elongation. The shape of the relaxation curve for a given molecular weight is the same at different temperatures, when plotted as reduced stress vs. logarithmic time; a change in temperature essentially shifts the position of the curve along the logarithmic time scale. The activation energy for relaxation, calculated by use of the Arrhenius equation, is found to be independent of molecular weight in the molecular weight range investigated (M̄v = 665,00.0 to 1,420,000), the average value being 15.4 kcal. Straight lines are obtained when reciprocal viscosity-average molecular weight is plotted against log time required for the reduced stress to reach a certain arbitrary value, at a fixed temperature and elongation. Relaxation rate depends on molecular weight with sufficient sensitivity so that relaxation measurements may be a practical method of measuring molecular weight directly in the solid state.
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    Journal of Polymer Science 3 (1948), S. 714-734 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
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    Journal of Polymer Science 3 (1948), S. 772-775 
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    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: Recently published data on copolymerization has been shown to correlate satisfactorily with the scheme of Q and e factors proposed by Alfrey and Price, thus lending further support to the utility and to the theoretical interpretation on which it was based.
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  • 68
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    Notes: The second-order transition temperatures (Tm) for foruteen commercially available butadiene-acrylonitrile copolymers with 18-50% acrylonitrile have been determined refractometrically and found to be somewhat lower than the corresponding brittle temperatrues (Tb). The data show a linear relation between Tm and acrylonitrile content.
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    Journal of Polymer Science 3 (1948), S. 897-898 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
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    Journal of Polymer Science 3 (1948), S. 899-900 
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    Keywords: Chemistry ; Polymer and Materials Science
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    Journal of Polymer Science 3 (1948), S. 141-142 
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    Keywords: Chemistry ; Polymer and Materials Science
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    Journal of Polymer Science 3 (1948), S. 143-143 
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    Journal of Polymer Science 3 (1948), S. 143-144 
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    Keywords: Chemistry ; Polymer and Materials Science
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  • 74
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    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The initial rate of polymerization of highly purified styrene in bulk has been measured dilatometrically at 38.4, 56.4 and 70.1°C. For conversions up to one per cent a well-reproducible rate was observed for samples handled in complete absence of atmospheric gases. For samples saturated with air an equally reproducible, though higher rate, was observed initially. The duration of this higher rate decreases with increasing length of storage between saturation and measurement. After polymerization at higher rate, the sample continues to polymerize at the rate observed for the air-free samples.
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  • 75
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    Journal of Polymer Science 3 (1948), S. 22-31 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: A turbidimetric method has been developed for determining the styrene content in water and soap solution. The solubility of styrene in distilled water was 0.022% while in 2.0% potassium oleate solution it was 0.65 to 0.88%. The course of the polymerization of a saturated solution of styrene in 2% potassium oleate was followed by a colorimetric analysis based on reaction with dilute potassium permanganate. The rate of polymerization decreased rapidly after 50% conversion. The activation energy was estimated to be 17,000 kcal., somewhat less than in solution. The molecular weight of the polymer produced was 200,000. Occasional erratic results were ascribed to possible influence of various amounts of air sealed in the polymerization mixtures.
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  • 76
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    Topics: Chemistry and Pharmacology , Physics
    Notes: It has been demonstrated that the homogeneity in respect to molecular weight of emulsion copolymers of butadiene and styrene can be increased by the use of certain derivatives of n-dodecyl mercaptan rather than the mercaptan itself. These derivatives decompose and relase n-dodecyl mercaptan at an even rate during the polymerization reaction. Several new derivatives of n-dodecyl mercaptan are described.
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  • 77
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    Topics: Chemistry and Pharmacology , Physics
    Notes: Precise analytical methods are developed using iodine monochloride for the determination of unsaturation in polybutadiene and polyisoprene and their copolymers with styrene. The complicating side reactions, splitting out and substitution, as well as the influence of the solvent employed are investigated in detail. It is concluded that GR-S at various conversions has the theoretical unsaturation. Emulsion polybutadiene exhibits 97 to 98% of the theoretical unsaturation, emulsion polyisoprene 97% sodium polybutadiene 92%, and sodium polyisoprene 85%. The amount of unsaturation in these last two polymers as well as in the sodium copolymer of butadiene and styrene (75:25) is considerable less than theoretically expected.
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  • 78
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    Keywords: Chemistry ; Polymer and Materials Science
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    Topics: Chemistry and Pharmacology , Physics
    Notes: Crystalline soybean trypsin inhibitor has been inactivated by ultraviolet light (λ2537 Å.) with a quantum yield of 0.0088 based upton loss of ability to inhibit the action of trypsin on casein. Inactivation involves a “one-hit” process.
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    Journal of Polymer Science 3 (1948), S. 303-303 
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    Keywords: Chemistry ; Polymer and Materials Science
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  • 80
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: Solid polyhexamethylene adipamide prepared by slow cooling of a melt is opaque as a result of formation of spherulites. Spherulites may also be formed by slow evaporation of a phenol solution of polyhexamethylene adipamide. Transparent, nonspherulitic polymer of a low degree of lateral order can be formed by cooling the polymer rapidly. Heat treatment or aging of this polymer increases the lateral order without the formation of microscopically visible spherulites. Spherulites usually reduce tensile strength, increase opacity, and decrease workability.
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    Journal of Polymer Science 3 (1948), S. 325-326 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Description / Table of Contents: The rate constants for thermal polymerization of indene at 150° and 175° in the absence of oxygen have been found to be 6.0 × 10-6 and 3.16 × 10-5 min.-1, respectively. The average degree of polymerization at each temperature was slightly less than four.
    Notes: Die Geschwindigkeitskonstante der thermischen Polymerisation von Inden bei 150° und 175° in Abwesenheit von Sauerstoff wird zu 6.0 × 10-6 und 3.16 × 10-5 min.-1 resp., bestimmt. Der durchschnittliche mittlere Polymerisationsgrad war etwas geringer als 4 bei beiden Versuchstemperaturen.
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    Journal of Polymer Science 3 (1948), S. 358-364 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The densities of undrawn and drawn nylon filaments (6-6 Nylon) are found to be 1.1339 and 1.1384, respectively, at 25°C. Annealing either the drawn or undrawn forms to the highest temperature possible short of melting increases the room temperature density to 1.1564, the most rapid increase in density with temperatures annealing coming at 210°C. The temperature coefficient of the density as measured at room temperature is greater for the drawn form of the nylon than the undrawn after annealing has taken place. The density of nylon calculated by Bunn and Garner from x-ray diagram data is 1.24, considerably higher than the highest value obtained by us on annealing, namely 1.156.
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    Journal of Polymer Science 3 (1948), S. 365-370 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Description / Table of Contents: A brief review is given of the evidence for the existence of a long period of about five hundred glucosidic units in fibrous cellulose. The heterogeneity of the molecular weight distribution can be measured as a function of the extent of degradation and is found to increase much less rapidly than would result from random scission. The interpretation of kinetic studies by means of Ekenstam's equation leads to the evaluation of two different rate constants and activation energies in the degradation reaction. Finally, the electron microscope photographs reveal significant difference between individual fibers resulting from wet milling and those produced by hydrolytic reaction.
    Notes: Eine Übersicht wird gegeben für die Argumente, die für das Vorhandensein eines regelmässigen, langperiodischen Aufbaus von Einheiten von 500 Glukoseresten in Fasercellulosen sprechen. Die Uneinheitlichkeit des Gewichtsdurchschnittes kann in ihrer Abhängigkeit vom Abbaugrad gemessen werden und nimmt viel langsamer ab als unter der Annahme von statistischer Spaltung. Die Interpretierung der kinetischen Studien mit Hilfe der Gleichung von Ekenstam führt zu zwei verschiedenen Geschwindigkeitskonstanten und Aktivierungsenergien für die Zerfallsreaktion. Schliesslich zeigen elektronenmikroskopische Aufnahmen charakteristische Unterschiede zwischen Fasern die durch Nassmahlung und durch Hydrolyse gewonnen wurden.
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  • 84
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    Topics: Chemistry and Pharmacology , Physics
    Notes: The inhibiting action of several phenols on the GR-S 10 (rosin soap) recipe for synthetic 2,5-Di-t-butylhydroquinone is shown to be a particularly powerful inhibitor rubber is reportor in this recipe.
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  • 85
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  • 86
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    Journal of Polymer Science 3 (1948), S. 464-464 
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    Keywords: Chemistry ; Polymer and Materials Science
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  • 87
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    Topics: Chemistry and Pharmacology , Physics
    Notes: An expression for the amount of chain transfer occurring in a copolymerization carried out in solvent media can be derived in a manner similar to the composition-kinetic treatment for tripolymer formation. As a result, the relative reactivity of the chain-transfer solvent can be determined.
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  • 88
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    Journal of Polymer Science 3 (1948), S. 465-480 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The fine structures of emulsion polybutadiene prepared at temperatures ranging from 55°C. to -20°C. and of various butadiene-styrene copolymers prepared at -20°C. have been studied by x-ray methods. The ability of emulsion-polymerized butadiene to crystallize was found to depend to a large extent on the temperature of polymerization. Butadiene polymerized at 30°C. and above showed no evidences of crystallization when cooled unstretched to -70°C. as observed by x-ray diffraction methods; however, butadiene polymerized at 20°C. and below showed crystallization effects when cooled unstretched to -70°C. These crystallization effects became more pronounced for samples polymerized at lower temperatures. Layer-line diffraction patterns of butadiene polymerized at 30°C. and below were obtained by stretching the polymer at about 0°C. From these patterns the geometrical repeat distance along the polymer chains was found to be 5.1 ± 0.1 Å. This corresponds to a fully extended butadiene unit in the trans configuration. An anomaly was observed in the diffraction patterns of crystallizable polybutadiene stretched at 0°C. Some of the layer-line spots varied in position with per cent elongation of the sample. This suggests that the molecules in crystallites of the polymer are inclined to the stretch axis at low elongations and that they become more nearly parallel to the stretch axis at higher elongations. A small addition of styrene as comonomer at -20°C. polymerization temperature did not prevent crystallization and preferred orientation effects in the polymer, since these effects could still be found in a 90/10 charge copolymer. Larger amounts of styrene did prevent crystallinity and preferred orientation as shown by the amorphous nature of an 80/20 charge copolymer. The ability of a compounded vulcanizate of a given polymer to crystallize is less than that of the purified polymer under the same conditions. This may be due to the combined effects of milling, vulcanization, and the presence of carbon black particles in the polymer. A description of the apparatus and techniques used for cooling and stretching these polymers is given.
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    Journal of Polymer Science 3 (1948), S. 503-517 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The rates of decomposition of benzoyl, lauroyl, bis(p-chlorobenzoyl), and bis(2,4-dichlorobenzoyl) peroxides, 0.0133 molar in styrene, have been determined at 34.8, 49.4, 61.0, 74.8, and 100°C., and the corresponding rates of polymerization of styrene have also been determined. Assuming the initial rate of polymerization of styrene, produced by benzoyl peroxide at an initial concentration of 0.0133 m./l. at each of the five temperatures used to be unity, the relative initial rates of polymerization produced by the peroxides studied are as follows: bis(2,4-dichlorobenzoyl) 2.15, lauroyl 1.52, and bis(p-chlorobenzoyl) 0.87. The rate data have been subjected to an approximate kinetic analysis, from which one may conclude that the order of intrinsic effectiveness of the peroxides as chain-initiating agents in styrene is benzoyl 〉 bis(p-chlorobenzoyl) 〉 lauroyl 〉 bis(2,4-dichlorobenzoyl), and that the effectiveness increases with increasing temperature. The activation energy for the peroxide-initiated polymerization of styrene was found to be 21 kcal. per mole. The molecular weight of polystyrene appears to be an inverse function of the temperature, the polymerization rate, the peroxide decomposition rate, and the extent of wasteful decomposition of the peroxide.
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    Journal of Polymer Science 3 (1948), S. 535-538 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Description / Table of Contents: A sample of polyindene (number average molecular weight, 400) was carefully fractionated into nine fractions with molecular weights varying from 300 to 800. The observation by Whitby and Katz that bromine titration indicated one double bond per polymer molecule was substantiated. However, this double bond is no longer active for polymerization since the molecular weights of various fractions did not change significantly on exposure to polymerizing conditions (heating for 500 hours under nitrogen at 175°C.).
    Notes: Eine Probe von Polyindol (mittleres Molekulargewicht 400) wird sorgfältig in 9 Fraktionen von steigendem Molekulargewicht von 300 bis 800 zerlegt. Die Beobachtung von Whitby und Katz, dass Bromtitrierung zu einer Doppelbindung pro Polymermolekül führt wird bestätigt. Diese Doppelbindung ist aber nicht länger zur Polymerisation fähig, da sich die Molekulargewichte verschiedener Fraktionen nicht mehr wesentlich änderten, wenn sie Polymerisationsbedingungen - Erhitzen für 500 Stunden bei 175° in Stickstoffatmosphäre - ausgesetzt wurden.
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    Journal of Polymer Science 3 (1948), S. 539-548 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The evidence for the nature of the side chains in lignin resulting from investigations of the reactions of model substances has been summarized. The studies have involved investigation of the reactions with (a) sulfite, (b) alkali and nitrobenzene, and (c) hot alkali. (a)Reaction with sulfite occurs readily for model substances with β-hydroxyl or α,β unsaturated keto groupings (“aldol type”). Hydroxyl groups adjacent to a ring are somewhat reactive but or-hydroxyketo groupings (“acyloin type”) do not react.(b)Alkaline oxidation to aldehyde or carboxyl with nitrobenzene is effective in degrading a side chain para to a free hydroxyl group having an oxygen atom on the α-carbon atom. Conversion of the para-phenolic hydroxyl to a methyl ether neutralizes its promoting influence.(c)Cleavage to an aldehyde with hot alkali in the absence of air is specific for the “aldol type” grouping in the side chain. This is regarded as a reverse aldol condensation and it has been demonstrated that acetaldehyde can be isolated from such degradations.These results, together with the behavior of lignin and its derivatives, are interpreted in terms of probable structures for the side-chain units in lignin.
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    Journal of Polymer Science 3 (1948), S. 602-603 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
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    Journal of Polymer Science 3 (1948), S. 603-604 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
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  • 94
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    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: A large-scale precise fractionation of GR-S (X-55) was performed using the fractional precipitation technique at 25°C. 9 fractions, each weighing approximately 150 g. and comprising approximately 11% by weight of the original unfractionated sample, were obtained and a detailed study was made showing the effect of number-average molecular weight and related sol-gel properties on various physical and chemical properties of the crude and vulcanized fractions. Using a Santocure tread-type recipe, preliminary compounding work indicated the sulfur ratios required to give vulcanizates with 300% modulus values of 1000 p.s.i. All fractions were recompounded using these indicated optimum sulfur values. Generally, as the number-average molecular weight increased, better stress-strain and quality index data were obtained. These and other physical properties of the vulcanizates of these fractions are discussed in detail. As found in past fractionation studies pertaining to unsaturated high polymers, the higher molecular weight fractions, obtained from the unfractionated sample which was totally soluble in benzene, undergo considerable gelation when isolated and vacuum dried at 25°C. in the dark. As the indicated molecular weight of the fraction increased, higher per cent gel contents were obtained. Compared to unfractionated butadiene-styrene copolymers of similar gel contents, the gel portions of the higher molecular weight fractions had unusually high swelling indices. indicating qualitatively that the average molecular weights between points of effective cross linking in the three-dimensional gel structure were higher than those encountered in the past in unfractionated samples of similar gel contents. Other data are given pertaining to these fractions, such as the bound styrene content, per cent shrinkage of the compounded unvulcanized stocks, and the rate of gel breakdown with cold milling.
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    Journal of Polymer Science 3 (1948), S. 607-608 
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    Keywords: Chemistry ; Polymer and Materials Science
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    Journal of Polymer Science 3 (1948), S. 642-645 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Description / Table of Contents: Polymeric oxidation products of indole act like typical peroxides in polymerization reactions. Due to their relatively high stability the increases of the reaction is small, while fragments of the degraded peroxide enter the polymer molecule.
    Notes: Polymere Oxydationsprodukte des Indens verhalten sich in Bezug auf Polymerisationsreaktionen wie typische Peroxyde. Ihre verhältnismässig hohe Stabilität bedingt eine relative geringe Reaktionsbeschleunigung, wobei Bruchstücke des zerfallenden Peroxyds in die polymere Molekel eintreten.
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    Journal of Polymer Science 3 (1948), S. 646-646 
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    Keywords: Chemistry ; Polymer and Materials Science
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  • 98
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    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: A refractometric technique for determination of second-order transition temperatures (Tm) of polymers has been extended to include a series of alkyl acrylate and methacrylate polymers with transitions at temperatures down to -50°C. A convenient technique for determining refractive index down to -75°C. is described. Certain long-chain alkyl polymers are birefringent below Tm. Correlations of brittle point with Tm and relations between viscosity and Tm are reported.
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    Journal of Polymer Science 3 (1948), S. 663-668 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
    Notes: The Verdet constants of nine polyethylene glycols, three polypropylene glycols, and nine silicone polymers have been measured at 25°C. It was found that the Verdet constant increases with increase in molecular weight in each of the series, and approaches a constant value. A similar increase in the molecular magnetic rotation was noted. The results are in contrast with those on polystyrene, and the effect of end groups on the measurements is discussed in explanation.
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    Journal of Polymer Science 3 (1948), S. 798-798 
    ISSN: 0022-3832
    Keywords: Chemistry ; Polymer and Materials Science
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Physics
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