The steady state flight performance of the Parafoil is computed by using aerodynamic coefficient data obtained from wind tunnel tests of both small scale models and full scale aspect ratio 2.0 units. The actual free flight performance of the Parafoil is obtained from both manned ascending flights and manned jumps from aircraft. Attention is also given to the flight stability and control of the Parafoil and to its unique landing flare. The agreement between the performance predictions based on the wind tunnel data and the results obtained from actual flight tests is presented. The performance of a more advanced aspect ratio 3.0 Parafoil design is considered. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Parafoil Flight Performance


    Beteiligte:
    J. D. Nicolaides (Autor:in) / M. A. Tragarz (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    70 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Parafoil flight performance

    NICOLAIDES, J. | AIAA | 1970


    Parafoil Powered Flight Performance

    J. D. Nicolaides | NTIS | 1972


    Parametric Study of Powered Parafoil Flight Dynamics

    Ward, M. / Culpepper, S. / Costello, M. et al. | British Library Conference Proceedings | 2012


    Parametric Study of Powered Parafoil Flight Dynamics

    Ward, Michael / Culpepper, Sean / Costello, Mark | AIAA | 2012


    Parafoil Flight Mechanics: A Novel Flight Test Facility

    Redelinghuys, Christiaan / Grunwald, Arthur / Rhodes, Steven et al. | AIAA | 2015