Flying at very high speeds results in excessive resistance, surface heating, and indeterminate character of flow at Mach numbers between 0.85 and 1.2; analysis of types of airfoils that will be needed, powers required and what must be done to overcome problems of friction and extremely high altitude heating effects; new problems of high altitude flight are ionization of air, meteoric dust, and electrification of atmosphere. (See also - n 11 Nov 1945 p 131-4)


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    Title :

    Analyzing aspects of future flight


    Additional title:

    Aviation


    Contributors:

    Published in:

    Aviation ; 44 , n 12 ; p 158-162


    Publication date :

    1945


    Size :

    5 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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