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  • AIRCRAFT  (1)
  • AIRCRAFT INSTRUMENTATION  (1)
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  • 1
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    Unknown
    Wind tunnel investigation of an all flush orifice air data system for a large subsonic aircraft (1980)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The results of a wind tunnel investigation on an all flush orifice air data system for use on a KC-135A aircraft are presented. The investigation was performed to determine the applicability of fixed all flush orifice air data systems that use only aircraft surfaces for orifices on the nose of the model (in a configuration similar to that of the shuttle entry air data system) provided the measurements required for the determination of stagnation pressure, angle of attack, and angle of sideslip. For the measurement of static pressure, additional flush orifices in positions on the sides of the fuselage corresponding to those in a standard pitot-static system were required. An acceptable but less accurate system, consisting of orifices only on the nose of the model, is defined and discussed.
    Keywords: AIRCRAFT INSTRUMENTATION
    Type: NASA-TP-1642 , H-1085
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
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    Unknown
    Tabulated pressure measurements on a large subsonic transport model airplane with high bypass ratio, powered, fan jet engines (1972)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: An experimental wind-tunnel investigation to determine the aerodynamic interference and the jet-wake interference associated with the wing, pylon, and high-bypass-ratio, powered, fan-jet model engines has been conducted on a typical high-wing logistics transport airplane configuration. Pressures were measured on the wing and pylons and on the surfaces of the engine fan cowl, turbine cowl, and plug. Combinations of wing, pylons, engines, and flow-through nacelles were tested, and the pressure coefficients are presented in tabular form. Tests were conducted at Mach numbers from 0.700 to 0.825 and angles of attack from -2 to 4 deg.
    Keywords: AIRCRAFT
    Type: NASA-TM-X-2530 , L-8182
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
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