Use of tension structure concept for flexible wings offers means of recovering and landing spacecraft; other uses include cargo towing and dropping, rocket booster recovery, power reconnaissance drone, and manned utility vehicle; data presented summarize recent aerodynamic information obtained at Langley Research Center; state of art with regard to lift-drag ratio with emphasis on fundamental factors affecting performance, stability, and control of parawing configurations; results of related studies and some comparisons with conventional wing theory.


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    Titel :

    Parawing aerodynamics


    Weitere Titelangaben:

    Astronautics Aerospace Eng


    Beteiligte:


    Erscheinungsdatum :

    1963


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    PARAWING AERODYNAMICS

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


    Large parawing development project

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


    Parawing Aercab Feasibility Flight Demonstration

    R. W. Speth / J. L. Rust / A. V. Coles | NTIS | 1971



    Parawing precision aerial delivery system

    BAIR, H. / FOREHAND, J. | AIAA | 1968