Wind tunnel investigation of high lift capabilities of 2 supersonic configurations equipped with stowable, fabric wings of parachute like construction that may be used for takeoff and landing; use of parawing resulted in threefold increase in lift coefficient at aircraft attitude of 12°; static lateral stability characteristics of canard model were improved by adding parawing.


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    Titel :

    Exploratory study of parawing as high-lift device for aircraft


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Naeseth, R.L. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Parawing aerodynamics

    Sleeman, Jr., W.C. / Johnson, Jr., J.L. | Engineering Index Backfile | 1963


    Ultra-light competitive titanium alloy parawing aircraft

    LEI XIAOJUN / LI XIAOPENG / WANG SUOMAO et al. | Europäisches Patentamt | 2020

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    PARAWING AERODYNAMICS

    Johnson, J. L., Jr. / Sleeman, W. C., Jr. | NTRS | 1963


    Large parawing development project

    Clemmons, D. L., Jr. | NTRS | 1967