Paper emphasizes great potential value of flight testing as means of conducting research into problems of high speed flight and shows that there is still much to be done if one is to understand fully all that occurs even at comparatively modest Mach numbers (up to, say, 0.85); compresssibility effects on drag and on lift; stability and control. (See also - discussion p 503-12)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Flight research at high subsonic speeds


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Davies, H. (author)

    Published in:

    Publication date :

    1948


    Size :

    21 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :