Tests of parachutes on six models of typical fighter and trainer airplanes. (Originally issued as Advance Restricted Report L5G19a Mar 1946)


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    Title :

    Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in Langley 20-foot freespinning tunnel, R


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1946


    Size :

    25 pages


    Remarks:

    27 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



    Wing parachutes for recovery from the spin

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    Tests of full-scale horizontal tail surface in Langley 16-foot high-speed tunnel

    Schueller, C.F. / Korycinski, P.F. / Strass, H.K. | Engineering Index Backfile | 1946


    Tests of a full-scale horizontal tail surface in the Langley 16-foot high-speed tunnel

    Schueller, Carl F. / Korycinski, Peter F. / Strass, H. Kurt | TIBKAT | 1946


    Tests of a Full-scale Horizontal Tail Surface in the Langley 16-foot High-speed Tunnel

    Schueller, Carl F / Korycinski, Peter F / Strass, H Kurt | NTRS | 1946