The results of an experimental program conducted in order to compile a data base useful in the application of airbreathing propulsion to missiles are presented. The configurations investigated used two-dimensional or axisymmetric twin inlets located at three alternative circumferential positions: 90, 115 and 135 deg to the vertical centerline. The effects of a wing located above the inlets and of various tail configurations were investigated, with a view to longitudinal stability/control and lateral-directional stability characteristics. It is noted that of the three tail configurations tested, the 'X' tail showed (1) the most linear pitch-moment curve, (2) control effectiveness, and (3) positive lateral-directional stability.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic characteristics of a series of airbreathing missile configurations


    Beteiligte:
    Hayes, C. (Autor:in)

    Kongress:

    Symposium on Aeroballistics ; 1981 ; Carderock, MD


    Erscheinungsdatum :

    01.05.1981


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamic and Inlet Flow Characteristics of Several Hypersonic Airbreathing Missile Concepts

    James L. Dillon / Don C. Marcum Patrick J. Johnston / James L. Hunt | AIAA | 1981


    Aerodynamic and inlet flow characteristics of several hypersonic airbreathing missile concepts

    Dillon, J. L. / Marcum, D. C., Jr. / Johnston, P. J. et al. | NTRS | 1980



    Aerodynamic and inlet flow characteristics of several hypersonic airbreathing missile concepts

    DILLON, J. / MARCUM, JR., D. / JOHNSTON, P. et al. | AIAA | 1980


    Hypersonic Airbreathing Missile

    Hunt, J. L. / Lawing, P. L. / Marcum, D. C., Jr. | NTRS | 1978