This paper has established the models calculating aero-optic effect of the hypersonic flying vehicle, and using a new turbulence hypothesis model, which is on base of Johnson- King & k-(epsilon) equation. Then the calculating program was designed. In the last part, the calculating result was discussed.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Calculating aero-optic effect of turbulent flow on the hypersonic flying vehicle


    Beteiligte:
    Wan, Ziming (Autor:in) / Guo, Yonghong (Autor:in) / Chen, Dingchang (Autor:in) / Yin, Xingliang (Autor:in)

    Kongress:

    Propagation and Imaging through the Atmosphere IV ; 2000 ; San Diego,CA,United States


    Erschienen in:

    Erscheinungsdatum :

    17.11.2000





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Calculating aero-optic effect of turbulent flow on the hypersonic flying vehicle [4125-11]

    Wan, Z. / Guo, Y. / Chen, D. et al. | British Library Conference Proceedings | 2000



    Aero-Optic Distortion in Transonic and Hypersonic Turbulent Boundary Layers

    Wyckham, Christopher M. / Smits, Alexander J. | AIAA | 2009


    Comparison of Aero-Optic Distortion in Hypersonic and Transonic, Turbulent Boundary Layers with Gas Injection

    Wyckham, C. / Smits, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006


    Measurement of Aero-Optic Distortion in Transonic and Hypersonic, Turbulent Boundary Layers with Gas Injection

    Wyckham, C. / Zaidi, S. H. / Miles, R. B. et al. | British Library Conference Proceedings | 2005