Series of lifting bodies has been tested at simulated high altitudes under hypersonic, cold-wall conditions; measurements of lift, drag, and static pitching moment were obtained over angle of attack range comparable to actual flight requirements; comparisons are made with modified Newtonian and free-molecular-flow theories; available theoretical and empirical techniques for analysis of transitional flow regime are reviewed and effect of lift-to-drag ratios varying with altitude is emphasized.


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    Title :

    Aerodynamics of typical lifting bodies under conditions simulating very high altitudes


    Additional title:

    AIAA J


    Contributors:
    Boylan, D.E. (author) / Potter, J.L. (author)

    Published in:

    AIAA Journal ; 5 , n 2 ; p 226-232


    Publication date :

    1967


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :