Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    NUMERICAL PREDICTION OF STAGNATION-POINT SHOCK-DETACHMENT DISTANCE FOR HYPERSONIC LOW DENSITY FLOW OVER BLUNT NOSE SHAPES



    Conference:

    24th, International congresss of aeronautical sciences ; 2004 ; Yokohama, Japan



    Publication date :

    2004-01-01


    Size :

    ICAS 2004-3.7.R.1


    Remarks:

    Also known as ICAS 2004.; HELD ON CD-ROM



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Study of Direct Gas Injection into stagnation zone of Blunt Nose at Hypersonic Flow

    Harmon, Peter / Vashishtha, Ashish / Callaghan, Dean et al. | AIAA | 2021


    STUDY OF DIRECT GAS INJECTION INTO STAGNATION ZONE OF BLUNT NOSE AT HYPERSONIC FLOW

    Harmon, Peter / Vashishtha, Ashish / Callaghan, Dean et al. | TIBKAT | 2021


    Stagnation-point heat transfer to blunt shapes in hypersonic flight, including effects of yaw

    Eggers, A. J. / Hansen, C. Frederick / Cunningham, Bernard E. | TIBKAT | 1958


    Shock Detachment Distance on Blunt Bodies in Nonequilibrium Flow

    Naoual Belouaggadia / Dr Tsutomu Hashimoto / Dr S Nonaka et al. | AIAA | 2007


    Induced pressures and shock shapes on blunt cones in hypersonic flow

    Wagner, Richard D. / Watson, Ralph | TIBKAT | 1964