Wind Tunnel tests conducted on model with pod mounted turbojet engines operating for lift augmentation during landing and takeoff; measurement of longitudinal aerodynamic characteristics over angles of attack from -8 to 16° for momentum coefficients from 0 to 2.0 at several trailing edge flap deflections with half and full span flaps.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic characteristics, temperature, and noise measurements of large-scale external-flow jet-augmented-flap model with turbojet engines operating


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Fink, M.P. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    46 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :