Digital computer study is made to investigate effects of differences in full scale aircraft and spin-tunnel-model testing techniques on spins and recoveries; results indicate that proper evaluation from spin-tunnel tests require cognizance of both tunnel technique and Reynolds number.


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    Title :

    Analytical investigation of effect of spin entry technique on spin and recovery characteristics for 60° delta-wing airplane


    Additional title:

    NASA -- Tech Note


    Contributors:
    Scher, S.H. (author) / Anglin, E.L. (author) / Lawrence, G.F. (author)


    Publication date :

    1959


    Size :

    52 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :