Approximate theories for supersonic and hypersonic flow over bodies of revolution at zero angle of attack are appraised by comparison with characteristics and second-order results, using hypersonic similarity as basis; combination of second-order supersonic and second-order shock-expansion theory provides good results; summary design curves give pressure drag of conical and ogive noses and boattails over transonic, supersonic, and hypersonic Mach numbers.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Summary of supersonic pressure drag of bodies of revolution


    Weitere Titelangaben:

    J Aerospace Sciences


    Beteiligte:
    Morris, D.N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Bodies of Revolution Having Minimum Drag at High Supersonic Airspeeds

    Dennis, David H / Resnikoff, Meyer M / Eggers, A J | NTRS | 1956


    Bodies of revolution having minimum drag at high supersonic airspeeds

    Eggers, Jr., A.J. / Resnikoff, M.M. / Dennis, D.H. | Engineering Index Backfile | 1956


    Minimum-drag bodies of revolution in nonuniform supersonic flow field

    Rennemann, Jr., C. | Engineering Index Backfile | 1955


    Bodies of revolution having minimum drag at high supersonic airspeeds

    Eggers, A. J. ;Resnikoff, Meyer M. ;Dennis, David H. | TIBKAT | 1957