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    Titel :

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


    Beteiligte:
    Harmon, Peter (Autor:in) / Vashishtha, Ashish (Autor:in) / Callaghan, Dean (Autor:in) / Nolan, Cathal (Autor:in) / Deiterding, Ralf (Autor:in)

    Kongress:

    AIAA Propulsion and Energy 2021 Forum



    Erscheinungsdatum :

    01.01.2021




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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

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


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

    Santos, W. F. N. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2004


    Stagnation heat flux estimation in spherically blunt axisymmetric hypersonic models

    Irimpan, Kiran J / Menezes, Viren | SAGE Publications | 2023


    Hypersonic Stagnation Line Merged Layer Flow on Blunt Axisymmetric Bodies of Arbitrary Shape

    Jain, A. C. / AIAA | British Library Conference Proceedings | 1993