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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    NASA -- Tech Note


    Contributors:
    Fink, M.P. (author)


    Publication date :

    1961


    Size :

    46 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :