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  • Industrial Chemistry  (500)
  • Aircraft Design, Testing and Performance  (21)
  • 1960-1964
  • 1950-1954  (521)
  • 1935-1939
  • 1952  (229)
  • 1951  (292)
Collection
Keywords
Publisher
Years
  • 1960-1964
  • 1950-1954  (521)
  • 1935-1939
Year
  • 1
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    Effect of Mach Number on the Flow and Application of Compressibility Corrections in a Two-Dimensional Subsonic-Transonic Compressor Cascade Having Varied Porous-Wall Suction at the Blade Tips (1952)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A cascade of 65-(12)10 compressor blades was tested at one geometric setting over a range of inlet Mach number from 0.12 to 0.89. Two groups of data are presented and compared: the first from the cascade operating conventionally with no boundary-layer control, and the second with the boundary layer controlled by a combination of upstream slot suction and porous-wall suction at the blade tips. A criterion for two-dimensionality was used to specify the degree of boundary-layer control by suction to be applied. The data are presented and an analysis is made to show the effect of Mach number on turning angle, blade wake, pressure distribution about the blade profile and static-pressure rise. The influence of boundary-layer control on these parameters as well as on the secondary losses is illustrated. A system of correlating the measured static-pressure rise through the cascade with the theoretical isentropic values is presented which gives good agreement with the data. The pressure distribution about the blade profile for an inlet Mach number of 0.21 is corrected with the Prandtl-Glauert, Karman-Tsien, and vector-mean velocity - contraction coefficient compressibility correction factors to inlet Mach numbers of 0.6 and 0.7. The resulting curves are compared with the experimental pressure distributions for inlet Mach numbers of 0.6 and 0.7 so that the validity of applying the three corrections can be evaluated.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-TN-2649
    Format: application/pdf
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  • 2
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    Empirical Relation Between Induced Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind-tunnel Tests on Four Model Rotors (1951)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The empirical relation between the induced velocity, thrust, and rate of vertical descent of a helicopter rotor was calculated from wind tunnel force tests on four model rotors by the application of blade-element theory to the measured values of the thrust, torque, blade angle, and equivalent free-stream rate of descent. The model tests covered the useful range of C(sub t)/sigma(sub e) (where C(sub t) is the thrust coefficient and sigma(sub e) is the effective solidity) and the range of vertical descent from hovering to descent velocities slightly greater than those for autorotation. The three bladed models, each of which had an effective solidity of 0.05 and NACA 0015 blade airfoil sections, were as follows: (1) constant-chord, untwisted blades of 3-ft radius; (2) untwisted blades of 3-ft radius having a 3/1 taper; (3) constant-chord blades of 3-ft radius having a linear twist of 12 degrees (washout) from axis of rotation to tip; and (4) constant-chord, untwisted blades of 2-ft radius. Because of the incorporation of a correction for blade dynamic twist and the use of a method of measuring the approximate equivalent free-stream velocity, it is believed that the data obtained from this program are more applicable to free-flight calculations than the data from previous model tests.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-TN-2474
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  • 3
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    A Flight Investigation of the Damping in Roll and Rolling Effectiveness Including Aeroelastic Effects of Rocket Propelled Missile Models Having Cruciform, Triangular, Interdigitated Wings and Tails (1951)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The damping in roll and rolling effectiveness of two models of a missile having cruciform, triangular, interdigitated wings and tails have been determined through a Mach number range of 0.8 to 1.8 by utilizing rocket-propelled test vehicles. Results indicate that the damping in roll was relatively constant over the Mach umber range investigated. The rolling effectiveness was essentially constant at low supersonic speeds and increased with increasing mach numbers in excess of 1.4 over the Mach number range investigated. Aeroelastic effects increase the rolling-effectiveness parameters pb/2V divided by delta and decrease both the rolling-moment coefficient due to wing deflection and the damping-in-roll coefficient.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-L51D16
    Format: text
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  • 4
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    Tank Investigation of the Grumman JRF-5 Airplane Equipped with Twin Hydro-Skis TED No. NACA DE 357 (1951)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: A tank investigation has been conducted on a 1/8-size powered dynamic model of the Grumman JRF-5 airplane equipped with twin hydro-skis. The results of tests using two types of skis are presented: one had vertical sides joining the top surface to the chine; the other had the top surface faired to the chine to eliminate the vertical sides. Both configurations had satisfactory longitudinal stability although the model had a slightly greater stable elevator range available when the skis without the vertical sides were attached. Free model tests indicated no instability present when one ski emerged before the other. Considerable excess thrust was available at all speeds with either type of skis. A hump gross load-resistance ratio of 3.37 was obtained with the skis with the vertical sides and 3.53 with the other skis. Landing behavior in smooth water with yaw up to 15deg and roll up to 15deg in opposite directions was satisfactory with either type of skis.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA RM-SL52D17
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  • 5
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    Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor. II - Effect on Over-All Performance Characteristics of Increasing Twelfth through Fifteenth Stage Stator-Blade Angles 3 deg (1952)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: The stator-blade angles in the twelfth through fifteenth stages of a 16-stage axial-flow compressor were increased 3O. The over-all performance of this modified compressor is compared to the performance of the compressor with original blade angles. The matching characteristics of the modified compressor and a two-stage turbine were obtained and compared to those of the compressor with original blade angles and the same turbine.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-E52A10
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  • 6
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    An Impulse-Momentum Method for Calculating Landing-Gear Contact Conditions in Eccentric Landings (1952)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: An impulse-momentum method for determining impact conditions for landing gears in eccentric landings is presented. The analysis is primarily concerned with the determination of contact velocities for impacts subsequent to initial touchdown in eccentric landings and with the determination of the effective mass acting on each landing gear. These parameters determine the energy-absorption requirements for the landing gear and, in conjunction with the particular characteristics of the landing gear, govern the magnitude of the ground loads. Changes in airplane angular and linear velocities and the magnitude of landing-gear vertical, drag, and side impulses resulting from a landing impact are determined by means of impulse-momentum relationships without the necessity for considering detailed force-time variations. The effective mass acting on each gear is also determined from the calculated landing-gear impulses. General equations applicable to any type of eccentric landing are written and solutions are obtained for the particular cases of an impact on one gear, a simultaneous impact on any two gears, and a symmetrical impact. In addition a solution is presented for a simplified two-degree-of-freedom system which allows rapid qualitative evaluation of the effects of certain principal parameters. The general analysis permits evaluation of the importance of such initial conditions at ground contact as vertical, horizontal, and side drift velocities, wing lift, roll and pitch angles, and rolling and pitching velocities, as well as the effects of such factors as landing gear location, airplane inertia, landing-gear length, energy-absorption efficiency, and wheel angular inertia on the severity of landing impacts. -A brief supplementary study which permits a limited evaluation of variable aerodynamic effects neglected in the analysis is presented in the appendix. Application of the analysis indicates that landing-gear impacts in eccentric landings can be appreciably more severe than impacts in symmetrical landings with the same sinking speed. The results also indicate the effects of landing-gear location, airplane inertia, initial wing lift, side drift velocity, attitude, and initial rolling velocity on the severity of both initial and subsequent landing-gear impacts. A comparison of the severity of impacts on auxiliary gears for tricycle and quadricycle configurations is also presented.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-TN-2596
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  • 7
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    Ditching Investigation of a 1/24-Scale Model of the Douglas C-124 Airplane (1951)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: An investigation of a 1/24- scale dynamically similar model of the Douglas C-124 airplane was made to determine the ditching characteristics and proper technique for ditching the airplane. Various conditions of damage, landing attitude, flap setting, and speed were investigated. The behavior of the model was determined from visual observations, motion- picture records, and time-history deceleration records. The results of the investigation are presented in table form, photographs, and curves. It was concluded on the basis of results from model tests with scale-strength bottoms (equivalent to 1150 pounds per square foot, full scale) that the airplane should be ditched at a medium nose-high landing attitude (near 7deg) with flaps full down. The airplane will probably make a smooth run with considerable damage resulting to the fuselage bottom just forward of the wing, but it is not likely that the water inflow will be overwhelming to personnel provided they are not in the belly compartment. Longitudinal decelerations in calm water will be about 2 1/2g and the landing run will be about four fuselage lengths.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-SL51F20
    Format: application/pdf
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  • 8
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    Structural Vulnerability of the Boeing B-29 Aircraft Wing to Damage by Warhead Fragments (1952)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: An elementary type of analysis has been used to determine the amount of wing tip that must be severed to produce irrevocable loss of control of a B-29 airplane. The remaining inboard structure of the Boeing B-29 wing has then been analyzed and curves are presented for the estimated reduction in structural strength due to four general types of damage produced by rod-type warhead fragments. The curves indicate the extent of structural damage required to produce a kill of the aircraft within 10 seconds.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-L52H01A
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  • 9
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    Free-Flight-Tunnel Investigation of the Dynamic Stability and Control Characteristics of a Chance Vought F7U-3 Airplane in Towed Flight (1952)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: As part of a program to determine the feasibility of using a fighter airplane as a parasite in combination with a Consolidated Vultee RB-36 for long-range reconnaissance missions (project FICON), an experimental investigation has been made in the Langley free-flight tunnel to determine the dynamic stability and control characteristics of a 1/17.5-scale model of a Chance Vought F7U-3 airplane in several tow configurations. The investigation consisted of flight tests in which the model was towed from a strut in the tunnel by a towline and by a direct coupling which provided complete angular freedom. The tests with the direct coupling also included a study of the effect of spring restraint in roll in order to simulate approximately the proposed full-scale arrangement in which the only freedom is that permitted by the flexibility of the launching and retrieving trapeze carried by the-bomber. For the tow configurations in which a towline was used (15 and 38 feet full scale), the model had a very unstable lateral oscillation which could not be controlled. The stability was also unsatisfactory for the tow configuration in Which the model was coupled directly to the strut with complete angular freedom. When spring restraint in roll was added, however, the stability was satisfactory. The use of the yaw damper which increased the damping in yaw to about six times the normal value of the model appeared to have no appreciable effect on the lateral oscillations in the towline configurations, but produced a slight improvement in the case of the direct coupling configurations. The longitudinal stability was satisfactory for those cases in which the lateral stability was good enough to permit study of longitudinal motions.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-SL53D07
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  • 10
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    The Design of Variable Mach Number Asymmetric Super-Sonic Nozzles by Two Procedures Employing Inclined and Curved Sonic Lines (1951)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: Two theoretical procedures are developed for designing asymmetric supersonic nozzles for which the calculated exit flow is nearly uniform over a range of Mach numbers. One procedure is applicable at Mach numbers less than approximately 3. This approach yields, without iteration, a nozzle for which the calculated exit flow is uniform at two Mach numbers and, with proper design, is nearly uniform at Mach numbers between, slightly above, and slightly below these two. The use of an inclined and curved sonic line is an essential feature of this approach, The second procedure requires iteration and is used far designs at Mach numbers exceeding 3. Although it is not a necessary feature, an inclined and curved sonic line is also used in this procedure. In both approaches the flow field dawn stream of the sonic line is determined using the method of characteristics.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-A51A19
    Format: application/pdf
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  • 11
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    Preliminary Results Obtained from Flight Test of a 1/7-Scale Rocket-Powered Model of the Grumman XF10F Airplane Configuration in the Swept-Wing Condition, TED No. NACA DE 354 (1951)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: A flight investigation of a 1/7-scale rocket-powered model of the XF10F Grumman XFl0F airplane in the swept-wing configuration has been made. The purpose of this test was to determine the static longitudinal stability, damping in pitch, and longitudinal control effectiveness of the airplane with the center of gravity at 20 percent of the wing mean aerodynamic chord. Only a small amount of data was obtained from the test because, immediately after booster separation at a Mach number of 0.88, the configuration was directionally unstable and diverged in sideslip. Simultaneous with the sideslip divergence, the model became longitudinally unstable at 3 degree angle of attack and -6 degree sideslip and diverged in pitch to a high angle of attack. During the pitch-up the free-floating horizontal tail became unstable at 5 degree angle of attack and the tail drifted against its positive deflection limit.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-SL52I25
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  • 12
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    Tank Investigation of the EDO Model 142 Hydro-Ski Research Airplane (1951)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: A tank investigation has been conducted of a 1/10-size powered-dynamic model of the Edo model 142 hydra-ski research airplane. The results of tests of two configurations are presented: One included a large ski and a ski well; the other, a small ski without a well. Water take-offs would be possible with the available thrust for either configuration: however, the configuration with the large ski emerged sooner and had less resistance from ski emergence until take-off. Longitudinal stability and landing behavior in smooth water were satisfactory for both configurations. Some alteration to the design of the tail would be desirable in order to reduce the spray loads.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-SL51I24
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  • 13
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    An Investigation of the Effect of the WADC 30,000-Horsepower Whirl Rig Upon the Static Characteristics of a Propeller (1952)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: Tests have been made at the Langley Aeronautical Laboratory on a 6000-horsepower propeller dynamometer installed at a ground test facility to determine the effect of a half-scale model of the Wright Aeronautical Development Center 30,000-horsepower whirl rig upon the aerodynamic characteristics of a three-blade NACA 10-(3)(062)-045 propeller. The model of the whirl rig was mounted in front of the 6000-horsepower propeller dynamometer. Static propeller tests were made for 0deg, 5deg, 10deg, 15deg, and 20deg blade angles over a range of rotational speeds from 600 to 2200 rpm in 100-rpm increments. Measurements were made of propeller thrust and torque, stresses in the propeller blades, and static and total pressures over the surface of the model. Propeller thrust and torque were increased up to 33 percent by the presence of the model of the whirl rig, but the average increase was from 5 to 10 percent. Blade vibratory stresses were small.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-SL52F20
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  • 14
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    A Wind-Tunnel Investigation to Determine the Effect of Various Head Designs on the Aerodynamic Characteristics in Pitch of the Army Ordnance Corps T205 3.5-Inch Heat Rocket (1952)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: The aerodynamic characteristics in pitch of the Army Ordnance Corps T205 3.5-inch HEAT rocket with various head designs and one fin modification have been determined at velocities of 500, 700 and 900 feet per second in the Langley high-speed 7- by 10-foot tunnel. The results presented are those of the full-scale model. Comparison of results obtained at 500 feet per second shows, in general, that for changes on the forward portion of the head the missile configurations having the greatest stability - most rearward center-of-loads location - were those having the highest drag. However, very limited comparisons indicate that the shape of the rear position of the head may be an important factor in reducing the drag and increasing the restoring moments. Generally, large increases in drag were noted for the various head designs with an increase in Mach number from 0.62 to 0.82. Pitching-moment-curve slopes increased with Mach number on all models except those having reasonably well-faired forward sections. These models showed a decrease in stability with increases in Mach number.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-SL52G15
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  • 15
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    Time-History Data of Maneuvers Performed by an F-86A Airplane During Squadron Operational Training (1952)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: Preliminary results of one phase of a control-motion study program are presented in the form of plots of load factor.and angular acceleration against indicated airspeed and of time histories of several measured quantities. The results were obtained from 197 maneuvers performed by an F-86A jet-fighter airplane during normal squadron operational training. Most of the tactical maneuver8 of which the F-86A is capable were performed at pressure altitudes ranging from 0 to 32,000 feet and at indicated airspeeds ranging from 95 to 650 miles per hour.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-L52C19
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  • 16
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    Force Characteristics in the Submerged and Planing Condition of a 1/5.78-Scale Model of a Hydro-Ski-Wheel Combination for the Grumman JRF-5 Airplane. TED No. NACA DE 357 (1952)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: Force characteristics determined from tank tests of a 1/5.78 scale model of a hydro-ski-wheel combination for the Grumman JRF-5 airplane are presented. The model was tested in both the submerged and planing conditions over a range of trim, speed, and load sufficiently large to represent the most probable full-size conditions.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-SLS2B28
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  • 17
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    Flow Over Inclined Bodies (1951)
    In:  CASI
    Details
    Publication Date: 2019-08-15
    Description: It has been shown that the circumferential pressure distributions for the inclined body and circular cylinder deviate from their respective theoretical inviscid distributions on the lee or downstream side in the same manner. With the aid of visual flow techniques, it has been shown that there is a shedding of vortices within the crossflow field of the inclined body. It has also been found that the vortex configuration depoends to a large extent on the shape of the nose of the body. To illustrate this, vapor screen pictures were made and results are discussed.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA Conference on Aerodynamic Design Problems of Supersonic Guided Missiles; Oct 02, 1951 - Oct 03, 1951; Moffett Field, CA; United States|Aerodynamic Characteristics of Bodies at Supersonic Speeds: A Collection of Three Papers; 31-44; NACA-RM-A51J25
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  • 18
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    The Effect of an Operating Propeller on the Aerodynamic Characteristics of a 1/10-Scale Model of the Lockheed XFV-1 Airplane at High Subsonic Speeds (TED No. NACA DE-377) (1952)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: An investigation was conducted in the Ames 12-foot pressure wind tunnel to determine the effect of an operating propeller on the aerodynamic characteristics of a l/l9-scale model of the Lockheed XFV-1 airplane, Several full-scale power conditions were simulated at Mach numbers from 0.50 to 0.92; the.Reynolds number was constant at 1,7 million. Lift, longitudinal force, pitch, roll, and yaw characteristics, determined with and without power, are presented for the complete model and for various combinations of model components, Results of an investigation to determine the characteristics of the dual-rotating propeller used on the model are given also,
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-SA52E06
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  • 19
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    Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor. III - Effect on Over-All Performance Characteristics on Increasing Stator-Blade Angles in Inlet Stages (1952)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: The stator-blade angles in the first four stages of a 16-stage axial-flow compressor were increased in order to decrease the angles of attack of these stages, and thereby to improve part-speed performance. The performance of this modified compressor was compared with that of the same compressor with original blade angles.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-E52B15
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  • 20
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    Investigation to Determine the Effectiveness of a Split-Aileron Type Emergency Spin-Recovery Device for the Northrop XF-89 Airplane (1951)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: The present paper presents the results of a brief investigation made to determine the effectiveness of a proposed emergency spin-recovery device to be used during demonstration spins of the Northrop XF -89 airplane. The proposed device makes use of split-type ailerons deflected +/-60deg on the outboard wing (left wing in a right spin). Tests made on a model which represented the airplane to a scale of 7 indicated that, if an uncontrollable spin is obtained in the design gross--weight loading, the device is not sufficiently effective to insure recovery,
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-SL-51H24
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  • 21
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    Error in Airspeed Measurement Due to Static-Pressure Field Ahead of the Wing Tip of a Swept-Wing Airplane Model at Transonic Speeds (1951)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: As part of a study of means of airspeed measurement at transonic speeds the use of static orifices located ahead of the wing tip has been investigated for possible application to service or research airspeed installations. The local static pressure and local Mach number have been measured at a distance of 1 tip chord ahead of the wing tip of a model of a swept-wing fighter airplane at true Mach numbers between 0.7 and 1.08 by the NACA wing-flow method. All measurements were made at or near zero lift. The local Mach number was found to be essentially equal to the true Mach numbers less than about 0.90. The local Mach number was found to be about 0.97 at a true Mach number of 0.95, and to be about 1.04 at a true Mach number of 1.08. The local Mach number provided a reasonable sensitive measure of true Mach number except for a restricted region near a true Mach number of 1.0 where the local Mach number did not change appreciably with true Mach number. The linear theory was found to predict qualitatively the effect of the fuselage on the static pressure ahead of the wing time but gave a reasonable prediction of the effect of the wing on the static pressure only at Mach numbers below 0.95.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-L50L28
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  • 22
    Electronic Resource
    Electronic Resource
    Masthead (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951) 
    Details
    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1002/cite.330230101
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  • 23
    Electronic Resource
    Electronic Resource
    Stabilität von Brennerflammen (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 4-4 
    Details
    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1002/cite.330230104
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  • 24
    Electronic Resource
    Electronic Resource
    Möglichkeiten einer Akustochemie (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 1-2 
    Details
    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Unter Akustochemie wird die Erzeugung von Schall beliebiger Frequenz durch chemische Energie und umgekehrt die Beeinflussung chemischer Reaktionen durch akustische Schwingungen verstanden. Schallsender mittels periodischer Explosionen, welche elektrisch, mechanisch oder durch Selbsterregung gesteuert sind, werden beschrieben.
    Additional Material: 5 Ill.
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1002/cite.330230102
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  • 25
    Electronic Resource
    Electronic Resource
    Korrosionsbeständigkeit legierter Stähle gegenüber reinem und schwefel-haltigem Kohlenoxyd (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 3-4 
    Details
    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Um den Einfluß von schwefel-haltigem Kohlenoxydgas zu ermitteln, wurden Proben aus verschiedenen Stahlsorten teils mit chemisch reinem, teils mit schwefel-haltigem Kohlenoxyd behandelt.
    Additional Material: 1 Ill.
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    Versammlungsberichte (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 15-16 
    Details
    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    URL: http://dx.doi.org/10.1002/cite.330230107
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    Umschau (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 16-21 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    Mehrstufige Gegenstromextraktion mit einem neuen Solvent-Zentrifugal-ExtraktorVorgetragen auf der Dechema-Hauptversammlung am 13. 7. 1950 in Frankfurt am Main. Sämtliche Tagungsvorträge erscheinen als Dechema-Monographie. (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 12-14 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Es wurde ein Extraktor entwickelt, der mehrere Extraktionsstufen in einem Aggregat vereinigt. Damit können schwierige Extraktionen in einem einzigen, lösemitteldichten Apparat durchgeführt werden, für die bisher Mischer und großräumige Absetzer oder mehrere Separatoren gebraucht wurden. Betriebserfahrungen über die Gewinnung von Penicillin werden mitgeteilt.
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    Normung (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 21-21 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    Einige Probleme des Stoff- und Wärmeüberganges an GrenzflächenErweiterte Fassung eines Vortrages in den Farbenfabriken Bayer, Leverkusen (17. 6. 1949) und in der Ruhrchemie A.G. Oberhausen-Holten (3. 1. 1950). (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 5-12 
    Details
    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Die im folgenden erörterten Fragen sind nicht nur deswegen Grenzprobleme, weil es sich bei ihnen um Transportvorgänge durch Phasengrenzen handelt. Vielmehr bildet dieses Gebiet auch eine Berührungsgrenze zwischen den Ingenieurwissenschaften und der physikalischen Chemie. Von erstgenannter Seite wurde der betreffende Fragenkreis in letzter Zeit mehrfach zusammenfassend dargestellt1. Hier möge er mehr vom Standpunkt der physikalischen Chemie aus und unter Bevorzugung der bisher noch nicht befriedigend gelösten Probleme behandelt werden. Gerade dieses Gebiet ist besonders geeignet, die Fruchtbarkeit einer Zusammenarbeit beider Wissenschaften im Rahmen der Verfahrenstechnik aufzuzeigen.
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    Neue Bücher (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 21-22 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Westdeutschlands chemische Industrie um die Jahreswende (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 23-24 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    Japans Soda- und Aetznatronindustrie in den Nachkriegsjahren (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 24-24 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Gewerblicher Rechtsschutz (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 27-27 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Tierkörperverwertung in Westdeutschland (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 24-25 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Wirtschaftsnachrichten (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 28-32 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Imperial Chemical Industries Ltd. im Jahre 1949 (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 25-26 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Masthead (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951) 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    Regelung von Destillationskolonnen (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 39-41 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: In der Praxis treten bei der Regelung von Destillations-Kolonnen immer wieder Schwierigkeiten auf, die nur durch eine enge Zusammenarbeit zwischen Betriebsingenieur und Regelungstechniker beseitigt werden können. In der vorliegenden Arbeit wird deshalb versucht, die Denk- und Arbeitsweise des Regelungstechnikers dem Verfahrensingenieur nahe zu bringen.
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    Entwicklungen der zerstörungsfreien WerkstückprüfungErweiterte und ergänzte Fassung eines Vortrages des Verfassers auf der Dechema-Informationstagung am 25. Juli 1949 in Frankfurt a. M. (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 33-38 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Notes: Die folgenden Ausführungen beschränken sich auf die Erörterung von Verfahren und Hilfsmitteln der zerstörungsfreien Werkstückprüfung, die in den letzten Jahren entstanden sind oder vervollkommnet wurden, und die die derzeitige Entwicklungstendenz erkennen lassen. Dabei werden die deutschen Kenntnisse, Erfahrungen und Arbeiten mit denen des Auslandes verglichen.
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    Versammlungsberichte (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 43-44 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Der Einfluß des Verschneidens auf die Lichtechtheit von Druckfarben für das graphische GewerbeInhalt eines Vortrages, gehalten am 15. März 1950, anläßlich einer Tagung des Fachnormenausschusses, ‚Farbe‘ in Berlin. Die Versuche wurden seinerzeit bei Kast & Ehinger, Stuttgart-Feuerbach, durchgeführt. (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 41-42 
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    Source: Wiley InterScience Backfile Collection 1832-2000
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    Notes: Die Kritik. an der bisherigen Bezeichnung der Lichtechtheit durch eine Zahl ohne Angabe der Konzentration ist berechtigt; denn selbst sehr lichtechte Druckfarben weisen eine Abhängigkeit der Lichtechtheit vom Farbstoffgehalt auf.
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    Umschau (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 44-47 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Neue Bücher (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 48-48 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Unfallverhütung (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 48-48 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Schwierige NE-Metallversorgung (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 49-50 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Zinnwirtschaft im Zeichen der Vorratskäufe (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 50-51 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Welterzeugung von Kolophonium und Terpentinöl (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 51-51 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Farben- und Lackerzeugung in Indien (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 52-52 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Masthead (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951) 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Wirtschaftsnachrichten (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 52-56 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Neue Apparaturen in der Salzsäure-Industrie (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 57-58 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Notes: Die Verwendung von Spezialgraphit hat bei Absorbern und Verbrennungsöfen für die Chlorwasserstoff-Synthese zu wesentlich leistungsfähigeren und raumsparenden Konstruktionen geführt, über die nachfolgend berichtet wird.
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    Die Wärmeleitfähigkeit von wäßrigen Lösungen starker Elektrolyte (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 59-64 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Notes: Die bisher vorliegenden Meßergebnisse für die Wärmeleitfähigkeit der wäßrigen Lösungen von Salzen, Säuren und Basen werden kritisch verglichen und in einheitlicher Form dargestellt. Auf Grund einfacher theoretischer Betrachtungen ist es möglich, diese wichtige Größe für zahlreiche noch nicht untersuchte Lösungen zuverlässig abzuschätzen.
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    Entwicklung der zerstörungsfreien Werkstückprüfung 2. Teil (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 65-68 
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    Source: Wiley InterScience Backfile Collection 1832-2000
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    Notes: Nachdem im ersten Teil dieser ArbeitI. Teil diese Ztschr. 23, 33 [1951]. die Durchstrahlungs-Verfahren und die magnetischen Verfahren der zerstörungsfreien Werkstückprüfung besprochen wurden, werden nachfolgend die elektrischen, akustischen, thermischen und chemischen Verfahren behandelt.
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    Einfluß eines Zusatzes auf die Verdampfungsgleichgewichte binärer Systeme(Nach Versuchen von G. G. Grau und E. Daubach) (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 64-64 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Notes: Es werden Verdampfungsgleichgewichte im System Äthanol-Wasser mit Salzzusätzen mitgeteilt, Messungen des Verdampfungsgleichgewichtes Methanol-Aceton unter Zusatz von CaCl2 und Glycerin, sowie Angaben über Verdampfungsgleichgewichte und Destillationsverhalten von Gemischen von Monomethylanilin und Dimethylanilin unter Zusatz von Glykol.
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    Versammlungsberichte (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 68-68 
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    Umschau (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 68-72 
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    Source: Wiley InterScience Backfile Collection 1832-2000
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    Chemische Verarbeitung von Körnerfruchtabfällen (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 73-75 
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    Unfallverhütung (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 72-72 
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    Fortfall der Produktionsbeschränkungen gefordert (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 75-76 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Neue Bücher (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 72-72 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    URL: http://dx.doi.org/10.1002/cite.330230308
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    Masthead (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951) 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    URL: http://dx.doi.org/10.1002/cite.330230401
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    Wirtschaftsnachrichten (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 76-80 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    URL: http://dx.doi.org/10.1002/cite.330230312
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    GraphitwärmeaustauscherVorgetragen auf der Tagung des Ausschusses für Wärmeforschung 1950 am 16. und 17. Oktober in Konstanz. (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 81-85 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Bei Wärmeaustauschern für korrodierende Medien mit relativ hohen Wärmeübergangswerten, wie diese bei der Verdampfung, Kondensation oder bei strömenden Flüssigkeiten auftreten, muß auch ein Werkstoff von hoher Wärmeleitzahl verwendet werden, damit wirtschaftlich vertretbare Einheiten gebaut werden können. Scheiden dafür aus korrosionstechnischen Gründen die üblichen Metalle und Legierungen aus, dann lassen sich innerhalb eines gewissen Druck- und Temperaturbereichs nun mit dem gas- und flüssigkeitsdicht imprägnierten Graphit Wärmeaustauscher hoher Flächenleistung bauen.
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    Versammlungsberichte (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 92-95 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    URL: http://dx.doi.org/10.1002/cite.330230405
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    Neuere Entwicklung der mechanischen Entstaubung im AuslandVorgetragen auf der Tagung des VDI-Fachausschusses für Staubtechnik am 30. März 1950 in Duisburg. (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 86-89 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Im Ausland ist das Bestreben erkennbar, von Großzyklonen zu Kleinzyklonen überzugehen, obwohl diese Bauart auch verschiedene Nachteile aufweist. Konstruktive Einzelheiten von Kleinzyklonen werden besprochen und abschließend die Staubabscheidung durch Ultraschall behandelt.
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    Laboratoriumsmethoden zur kontinuierlichen Trennung binärer azeotroper Systeme (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 90-92 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Es wurden einige Apparaturen entwickelt, um im Laboratoriumsmaßstab binäre azeotrope Systeme kontinuierlich zu trennen. Sie dienten zur experimentellen Überprüfung von Trennmethoden bei möglichst geringem Aufwand an Geräten, Energie und Chemikalien. In jedem der besprochenen Systeme ist die Erzielung höherer Reinheitsgrade und größerer Durchsätze nur eine Frage der Vergrößerung der Apparatur, ohne daß sich am Trennungsprinzip etwas ändert. Zur Überschreitung der azeotropen Konzentration wurden Entmischung infolge partieller Löslichkeit, Extraktion und die Verwendung einer Zusatzkomponente herangezogen.
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    Umschau (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 95-98 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Additional Material: 2 Ill.
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    URL: http://dx.doi.org/10.1002/cite.330230406
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    Neue deutsche Normen (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 98-98 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Neue Bücher (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 98-98 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Patentstreit um die Atombombe (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 99-99 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Rheniumgewinnnung in Ostdeutschland (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 99-100 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Wirtschaftsnachrichten (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 100-104 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    Masthead (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951) 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    URL: http://dx.doi.org/10.1002/cite.330230501
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    Zur Entwicklung der chemischen Technologie. Ernst Berl zum Gedächtnis (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 105-106 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Physikalisch-technische Eigenschaften von Kälteschutzstoffen (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 106-106 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Additional Material: 1 Tab.
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    Planung von Reaktionsöfen für heterogene Gaskatalysen (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 111-111 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    URL: http://dx.doi.org/10.1002/cite.330230505
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    Löslichkeit von Kohlenwasserstoffen verschiedenen Typs in Methanol und Benzylalkohol (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 112-113 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Im Laufe von Untersuchungen über die Phasengleichgewichte in ternären und polynären Systemen war es notwendig, die Löslichkeit von Kohlenwasserstoffen in Methyl- und Benzylalkohol zu untersuchen. Außer Gesichtspunkten allgemeiner Natur spielte bei dieser Arbeit auch die Erwägung eine Rolle, gegebenenfalls neue analytische und präparative Möglichkeiten zu gewinnen.
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    Kältebedarf von Vakuum-Xanthatknetern (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 113-115 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Um die Fragen nach dem Kältebedarf und der zweckmäßigsten Soletemperatur bei der Ausrüstung von Kunstfaserfabriken mit Kältemaschinenanlagen zu klären, wurden Untersuchungen an Xanthatknetern durchgeführt, über die nachstehend berichtet wird.
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    Zur Normung im ApparatebauNach dem Vortrag „Normalelemente und Aufbaugeräte“ auf der Dechema-Informationstagung 1949.  -  Die in dieser Arbeit besprochenen Fragen gewinnen dadurch an Aktualität, daß vor kurzem in Kassel die Gründungssitzung des Fachnormenausschusses „Chemischer Apparatebau“ stattgefunden hat, auf der Dr.-Ing. E. Mach, Ludwigshafen/Rhein, BASF, zum Vorsitzenden und der Autor dieser Arbeit zum stellvertretenden Vorsitzenden gewählt wurden. (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 107-111 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Notes: An zahlreichen Beispielen wird gezeigt, daß die Normung in der Verfahrenstechnik und im Apparatebau sich nicht allein auf Größe und Form von Flanschen, Rohren, Nieten und anderen Maschinenelementen beschränken darf, sondern daß sie zweckmäßigerweise auch ganze Apparaturen umfassen sollte.
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    Versammlungsberichte (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 116-117 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Normung (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 120-120 
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    Source: Wiley InterScience Backfile Collection 1832-2000
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    Neue Bücher (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 120-120 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Unfallverhütung (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 120-120 
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    Keywords: Chemistry ; Industrial Chemistry
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    Umschau (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 117-119 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Additional Material: 4 Ill.
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    Argentiniens Quebrachoindustrie gefährdet? (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 122-122 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Aus der Arbeit der BASF (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 121-122 
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    Source: Wiley InterScience Backfile Collection 1832-2000
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    Erzeugung von Phospor in USA (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 122-123 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Gewerblicher Rechtsschutz (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 123-123 
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    Wirtschaftsnachrichten (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 124-128 
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    Source: Wiley InterScience Backfile Collection 1832-2000
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    Masthead (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951) 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Zustand des Gases und nassen Gutes beim Trockenvorgang, mit Darstellung in einem geänderten Mollier-Diagramm feuchter Luft (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 129-134 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Das i, x-Bild feuchter Luft nach Mollier mit schiefwinkligen Koordinaten wird abgewandelt in ein Diagramm mit senkrechten Koordinaten. Unter Beibehaltung des gleichen graphischen Darstellungsfeldes wird dies dadurch möglich, daß der Wärmeinhalt auf ein gasförmiges Gemisch von 0 °C bezogen wird. Die Linien gleicher Kühlgrenze werden von einer Wärmebilanzgleichung ausgehend ermittelt. Ansatzgleichungen über den gekoppelten Wärme-und Stoffaustausch gestatteten ferner, zusätzlich in das neue Diagramm Linien einzutragen, die den geometrischen Ort aller Luftzustände darstellen, welche einem nassen Gut mit gleichem Wassergehalt und gleicher Temperatur zugeordnet sind.
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    Umschau (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 139-141 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Additional Material: 6 Ill.
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    Neue deutsche Normen (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 141-141 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Über ein neuzeitliches Festigkeitsproblem des ApparatebauesDer Verfasser hat die Arbeit seinem hochverehrten Kollegen, Herrn Prof. Dr.-Ing. Emil Kirschbaum, zu dessen 50. Geburtstag am 25. Juli 1950 gewidmet. (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 135-139 
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    ISSN: 0009-286X
    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: Bei dem in der vorliegenden Arbeit erstmalig gelösten Festigkeitsproblem handelt es sich um Fragen, die bei der Berechnung solcher Hochdruckrohre von Bedeutung sind, die im Gegensatz zu den bisher verwendeten geschmiedeten Massivrohren aus einem dünnwandigen Kernrohr bestehen, auf das  -  je nach der Höhe des Innendrucks  -  eine mehr oder weniger große Zahl von Bändern aufgewickelt wird. Außerdem spielt das Problem auch bei anders gearteten Aufgaben eine Rolle, auf die kurz hingewiesen wird.
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    Neue Bücher (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 142-142 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    Neue Zeitschriften (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 142-142 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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    Unfallverhütung (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 142-142 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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    Welterzeugung von Brom (1951)
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    Chemie Ingenieur Technik - CIT 23 (1951), S. 143-144 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
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  • 100
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    Ausbaupläne der französischen chemischen Industrie (1951)
    Weinheim : Wiley-Blackwell
    Chemie Ingenieur Technik - CIT 23 (1951), S. 145-146 
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    Keywords: Chemistry ; Industrial Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
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