Free stream and stagnation pressure measurement as principal means of determining air speed, Mach number, and altitude of aircraft; technique for compensating for deviation of measured static pressure at some location on aircraft from true free stream pressure, due to field of flow about aircraft; principle based on premise that it is possible to produce desired pressure variation with Mach number by proper choice of aerodynamic body shape and selection of location of pressure source on this body.


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    Titel :

    Aerodynamic means of static-pressure compensation for transonic and supersonic aircraft


    Weitere Titelangaben:

    Aeronautical Eng Rev


    Beteiligte:
    Korkegi, R.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1957


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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    Jehanzeb Masud / Adnan Latif / Shakil Sheikh et al. | AIAA | 2007


    Supersonic and transonic aircraft problems

    Reichert, C.E. | Engineering Index Backfile | 1950


    Euler Flow Analysis of Supersonic Transport Aircraft Configurations for Aerodynamic Optimization in Transonic and Supersonic Regimes

    De Nicola, C. / Tognaccini, R. / Amendola, A. et al. | British Library Conference Proceedings | 1994