Procedure for pilot escape from spinning airplanes has been determined by means of tests in which pilot escape was simulated from 21 airplane models spinning in the Langley 20-foot free-spinning tunnel. The results in general indicated that the pilot should bail out of the outboard side. Calculated centripetal accelerations acting on the pilot during a spin are presented.


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    Titel :

    Pilot Escape from Spinning Airplanes as Determined from Free-spinning-tunnel Tests


    Beteiligte:

    Erscheinungsdatum :

    01.10.1951


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch