An experimental investigation has been made in the Langley stability tunnel at low speed to determine the static longitudinal and lateral stability characteristics of a l/9-scale powered model of the Convair XFY-1 vertically rising airplane. Effects of thrust coefficient were investigated for the complete model and for certain components of the model. Effects of control deflections and of propeller-blade angle were investigated briefly for the complete model. Most of the tests were made through an angle-of-attack range from about -4 deg. to 29 deg, and the thrust-coefficient range was from 0 t o 0.7. In order to expedite distribution of these data to interested persons, no analysis of the data has been prepared for this report,


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    Titel :

    Wind-Tunnel Investigation at Low Speed of the Static Longitudinal and Lateral Stability Characteristics of a 1/9-Scale Powered Model of the Convair XFY-1 Vertically Rising Airplane


    Beteiligte:
    Queijo, M. J. (Autor:in) / Wolhart, W. D. (Autor:in) / Fletcher, H. S. (Autor:in)

    Erscheinungsdatum :

    11.02.1953


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch