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  • Other Sources  (1,345)
  • AIRCRAFT  (1,345)
  • 2015-2019
  • 1970-1974  (1,345)
  • 1
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    Aeronautical engineering: A special bibliography with indexes, supplement 38, December 1973 (1973)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: This special bibliography lists 473 reports, articles, and other documents introduced into the NASA scientific and technical information system in November 1973.
    Keywords: AIRCRAFT
    Type: NASA-SP-7037(38)
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    NASA propulsive lift STOL technology program (1973)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: A NASA propulsive-lift technology program for short takeoff aircraft is discussed. In the propulsive-lift program, turbofan engine power is used to augment the lift of essentially conventional wings. Potentially important applications of the propulsive lift developments for various aircraft operating conditions are reported. It is stated that the objective of the program is to provide technical information on the design, development, operation, and regulation of propulsive-lift aircraft.
    Keywords: AIRCRAFT
    Type: AGARD Mil. Appl. of V(STOL Aircraft, Vol. 1; 4 p
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    Recent NASA handling qualities research (1972)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: A comprehensive review of NASA research results documented since the mid-1960's and some recently completed programs on aircraft handling qualities are presented. In addition to handling qualities research pertaining to vehicle stability and control characteristics, investigations related to specialized piloting tasks, cockpit displays, and environmental factors are summarized. The background leading to NASA's handling qualities research activities is discussed, and programs that have received major emphasis are indicated. For general aviation aircraft, the survey includes investigations aimed at improving handling qualities by incorporating increasingly sophisticated stability augmentation and display systems, simplifying the approach and landing task for relatively inexperienced pilots, and establishing the basic effects of turbulence. Research on the specialized piloting problem of steeper instrument approaches for noise abatement and investigations with a representative first generation aircraft are reviewed in the section on subsonic jet transports. Supersonic cruise aircraft programs include a variety of simulation studies related to supersonic transport designs and flight tests with the XB-70 aircraft. Investigations of high angle of attack loss of control problems and a flight study of direct lift control utilization for formation flying and aerial refueling are discussed in the review of tactical military aircraft research.
    Keywords: AIRCRAFT
    Type: AGARD Handling Qualities Criteria; 25 p
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    Avoidance of Aircraft Trailing Vortex Hazards (1971)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: Safety measures to eliminate aircraft trailing vortex hazards
    Keywords: AIRCRAFT
    Type: NASA-TM-X-67125 , AGARD LESSONS WITH EMPHASIS ON FLIGHT MECH. FROM OPERATING EXPERIENCE, INCIDENTS AND ACCIDENTS MAR. 1971 (SEE N71-23410 12-02)
    Format: text
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    NASA TECHNICAL REPORTS
  • 5
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    Aeronautical Engineering - A special bibliography with indexes, supplement 4 (1971)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: Bibliographies of aeronautical engineering, design, production, evaluation, operation, and performance of aircraft and associated components equipment, and systems
    Keywords: AIRCRAFT
    Type: NASA-SP-7037(04)
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 6
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    Aircraft wake turbulence avoidance (1971)
    In:  CASI
    Details
    Publication Date: 2019-08-27
    Description: Analytical studies and flight tests are used to describe the formation and severity of trailing vortices and the spatial extent of their influence. This information is then used to outline procedures for ready application by pilots, tower operators, and others concerned with the flow of traffic. The procedures provide the necessary appreciation of the physical attributes of trailing vortices, the potential hazards involved when encountering them, and how best to avoid the dangerous portions of the wake during flight operations.
    Keywords: AIRCRAFT
    Type: NASA-TM-X-67448 , REPT-72/6 , Anglo-Am. Aeron. Conf.; Jul 07, 1971 - Jul 09, 1971; Calgary; Canada
    Format: application/pdf
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  • 7
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    A Structural Design for an Externally Blown Flap (EBF) Medium STOL Research Aircraft (1972)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: A computer program to predict, by reference to structural drawings, the dynamic response of a high lift STOL wing with externally blown flaps was developed. Structural data for the computer program are presented in the form of sketches, weight and dynamic loads information graphs, and tables for an external blown, triple-slotted flap, high lift STOL transport wing. Weight, mass distribution, and moment of inertia data are summarized in table form and presented pictorially by drawing layout. The methods used for obtaining weight data were: (1) actual know, weight of components, (2) preliminary stress sizing, and (3) statistical weight estimating methods.
    Keywords: AIRCRAFT
    Type: NASA-CR-112249
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 8
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    Cruise Drag Results from High Speed Wind Tunnel Tests of NASA Refan JT8D Engine Nacelles on the Boeing 727-200 (1973)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: High speed wind tunnel test results are presented showing the cruise drag effect of installing JT8D-109 Refan engines on a Boeing 727-200. Incremental drags of a refan center inlet and side nacelles are presented for several configuration variations. Static pressure distributions were obtained on the side nacelle strut and on the fuselage (above and below the strut). Oil flow photographs of selected configurations are also presented. In general the drag level of the refan installation is slightly better than predicted prior to the test and the drag rise is favorable.
    Keywords: AIRCRAFT
    Type: NASA-CR-134546 , D6-43099
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 9
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    A Flying Ejection Seat (1972)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: To increase aircrewmen's chances for safe rescue in combat zones, the armed forces are investigating advanced escape and rescue concepts that will provide independent flight after ejection and thus reduce the risk of capture. One of the candidate concepts is discussed; namely, a stowable autogyro that serves as the crewman's seat during normal operations and automatically converts to a flight vehicle after ejection. Discussed are (1) the mechanism subsystems that the concept embodies to meet the weight and cockpit-packaging constraints and (2) tests that demonstrated the technical feasibility of the stowage, deployment, and flight operation of the rotor lift system.
    Keywords: AIRCRAFT
    Type: NASA. Lyndon B. Johnson Space Center The 7th Aerospace Mech. Symp.; p 275-286
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 10
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    Some applications of buoyancy systems and parawings to replace conventional and proposed transportation systems. (1972)
    In:  Other Sources
    Details
    Publication Date: 2019-08-13
    Description: An exploratory study has been conducted to assess the performance potential of buoyant airships and parawings in short-haul passenger transportation. Results show that such systems can be used effectively, from a performance standpoint, in a VTOL or STOL mode of operation. A supplementary assessment of potential applications of such vehicles is examined, with a brief look at economic factors and an examination of missions for which they might be effectively used.
    Keywords: AIRCRAFT
    Format: text
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    NASA TECHNICAL REPORTS
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