Results of a numerical study of the supersonic high-enthalpy flow over a spherically blunt cone taking into account complicating factors are presented. These factors include simultaneous action of rotation of the body around the longitudinal axis and processes in ablating heat shield. The problem of body heating in a conjugate formulation is solved. At a nonzero angle of attack influence of an aircraft rotation with a small angular velocity (0–500 deg/s) on surface temperature distribution and heat and mass transfer is considered. The asymmetries of surface temperature and material removal via ablation on a rotating body were studied.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Rotation Influence on Heat Transfer at Supersonic Flow Around a Blunted Body



    Published in:

    AIAA Journal ; 56 , 2 ; 743-751


    Publication date :

    2018-02-01




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    The Pressure Drag of Blunted Cones in Supersonic Flow

    Eremenko, P. / Mouton, C. A. / Hornung, H. G. et al. | British Library Conference Proceedings | 2003


    Hypersonic flow around a spherically blunted cone

    Kamimoto, Goro / Kimura, Takeyoshi | TIBKAT | 1967



    Nonequilibrium flow expansion experiment around a blunted cone

    Kastell, D. / Horvath, T. J. / Eitelberg, G. | British Library Online Contents | 1995