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  • Analytical Chemistry and Spectroscopy  (665)
  • AERODYNAMICS  (299)
  • 1970-1974  (964)
  • 1974  (964)
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  • 1970-1974  (964)
Year
  • 1
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    Aeronautical Engineering: A special bibliography with indexes, supplement 48 (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: This special bibliography lists 291 reports, articles, and other documents introduced into the NASA scientific and technical information system in August 1974.
    Keywords: AERODYNAMICS
    Type: NASA-SP-7037(48)
    Format: application/pdf
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  • 2
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    Aeronautical Engineering: A special bibliography with indexes, supplement 47 (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: This special bibliography lists 185 reports, articles, and other documents introduced into the NASA scientific and technical information system in July 1974.
    Keywords: AERODYNAMICS
    Type: NASA-SP-7037(47)
    Format: application/pdf
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  • 3
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    Aeronautical engineering: A special bibliography, supplement 45, June 1974 (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: This special bibliography lists 430 reports, articles, and other documents introduced into the NASA scientific and technical information system in May 1974.
    Keywords: AERODYNAMICS
    Type: NASA-SP-7037(45)
    Format: application/pdf
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  • 4
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    Aeronautical engineering: A special bibliography with indexes, supplement 42, March 1974 (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: This special bibliography lists 338 reports, articles, and other documents introduced into the NASA scientific and technical information system in February 1974.
    Keywords: AERODYNAMICS
    Type: NASA-SP-7037(42)
    Format: application/pdf
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  • 5
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    Aeronautical engineering: A special bibliography with indexes, supplement 41, February 1974 (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: This special bibliography lists 514 reports, articles, and other documents introduced into the NASA scientific and technical information system in January 1974.
    Keywords: AERODYNAMICS
    Type: NASA-SP-7037(41)
    Format: application/pdf
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  • 6
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    A cumulative index to the 1973 issues of Aeronautical engineering: A special bibliography (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-27
    Description: This publication is a cumulative index to the abstracts contained in NASA SP-7037 (28) through NASA SP-7037 (39) of Aeronautical Engineering: A Special Bibliography. NASA SP-7037 and its supplements have been compiled through the cooperative efforts of the American Institute of Aeronautics and Astronautics (AIAA) and the National Aeronautics and Space Administration (NASA). This cumulative index includes subject, personal author, corporate source, contract, and report number indexes.
    Keywords: AERODYNAMICS
    Type: NASA-SP-7037(40) , NASA-SP-7037(28) , NASA-SP-7037(40)
    Format: application/pdf
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  • 7
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    Aircraft wake turbulence minimization by aerodynamic means (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-08-13
    Description: The paper reviews NASA's efforts on wake vortex turbulence minimization by aerodynamic design or retrofit modifications to large transport aircraft. Theoretical and experimental (ground-based and flight) results are presented which show that the adverse effects of a vortex wake produced by a large aircraft on a small following aircraft can be reduced significantly.
    Keywords: AERODYNAMICS
    Type: American Meteorological Society and American Institute of Aeronautics and Astronautics, Conference on Aerospace and Aeronautical Meteorology; Nov 12, 1974 - Nov 14, 1974; El Paso, TX
    Format: text
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  • 8
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    Technical evaluation report on AGARD Flight Mechanics Panel Symposium on Flight in Turbulence (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-13
    Description: The proceedings of a conference on the effects of atmospheric turbulence on flight characteristics are presented. The subjects discussed include the following: (1) turbulent environment, (2) operational problems, (3) design criteria, and (4) artificial aids for flight improvement. One conclusion is that there is a critical need for cross correlation measurements between various low atmosphere turbulence components. Additional discussion were held concerning wake vortex research for wake vortex detection and avoidance.
    Keywords: AERODYNAMICS
    Type: AGARD-AR-67 , May 14, 1973 - May 18, 1973; Woburn Abbey
    Format: text
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  • 9
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    Investigation of the stall-induced shock wave /hammershock/ at the inlet to the engine (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-07-27
    Description: The peak static pressures measured at the inlet to the engine during stall are presented for a turbojet and two turbofan engines. It is shown for one turbofan and the turbojet that the static pressure ratio across the hammershock does not exceed significantly the normal shock pressure ratio necessary to stop the flow. The second turbofan engine did not follow this rule. Possible reasons for the departure are discussed. For the two turbofan engines, the influence of the stall method on the hammershock intensity has been investigated. Data related to the spatial distribution of pressure in the hammershock are also presented.
    Keywords: AERODYNAMICS
    Type: Symposium on Propulsion System Structural Integration and Engineering Integrity; Sept. 3-6, 1974; Monterey, CA
    Format: text
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  • 10
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    Reynolds number effects on boattail drag of exhaust nozzles from wind tunnel and flight tests (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-07-27
    Description: A family of nacelle-mounted high-angle boattail nozzles was tested to investigate Reynolds number effects on drag. The nozzles were flown on a modified F-106B and mounted on scale models of an F-106 in a wind tunnel. A 19-to-1 range of Reynolds number was covered as a result of the large size differences between models and by flying over a range of altitude. In flight the nozzles were mounted behind J-85 turbojet engines. Jet boundary simulators and a powered turbojet engine simulator were used on the wind tunnel models. Data were taken at Mach numbers of 0.6 and 0.9. Boattail drag was found to be affected by Reynolds number. The effect is a complex relationship dependent upon boundary layer thickness and nozzle boattail shape. As Reynolds number was increased from the lowest values obtained with scale models, boattail drag first increased to a maximum at the lowest flight Reynolds number and then decreased.
    Keywords: AERODYNAMICS
    Type: Fluid Dynamics Panel Specialists Meeting on Airframe/Propulsion Interference; Sept. 3-6, 1974; Rome; Italy
    Format: text
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