This report presents results of an investigation carried out in the Naval Ordnance Laboratory's Supersonic Tunnel Number 1 to determine the aerodynamic characteristics of the AGARD Calibration Model B. Tests were conducted at free-stream Mach numbers ranging from 0.70 to 3.50, at angles of attack from -4 to +10 degrees, over a Reynolds number range from 0.20 times 100to the 6th power to 0.62 times 10 to the 6th power. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Wind Tunnel Measurements of the AGARD Calibration Model B at Transonic and Supersonic Speeds


    Beteiligte:
    J. B. Eades (Autor:in)

    Erscheinungsdatum :

    1964


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    AGARD wind tunnel calibration models

    Engineering Index Backfile | 1958


    Wind Tunnel Blockage Effects on the AGARD B Model in Transonic Flow

    Lombardi, G. / Morelli, M. | British Library Online Contents | 1994


    Wind Tunnel Blockage Effects on the AGARD B Model in Transonic Flow

    Lombardi, G. / Morelli, M. / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1994