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    Titel :

    HEAT FLUX MEASUREMENT OF APOLLO CAPSULE MODEL AT HIGH STAGNATION PRESSURE IN SHOCK TUNNEL HIEST (AIAA 2018-5264)


    Beteiligte:
    Tanno, Hideyuki (Autor:in) / Komuro, Tomoyuki (Autor:in) / Sato, Kazuo (Autor:in) / Itoh, Katsuhiro (Autor:in) / Matsumoto, Takehiro (Autor:in) / Yamamoto, Kosuke (Autor:in) / Tomita, Taketo (Autor:in) / Yoshitomi, Yuki (Autor:in)

    Kongress:

    AIAA International Space Planes and Hypersonic Systems and Technolgies (Conference)



    Erscheinungsdatum :

    2018-01-01


    Format / Umfang :

    7 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2018


    Heat Flux Measurement of Apollo Capsule Model in the Free-Piston Shock Tunnel HIEST

    Tanno, H. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2009


    Aeroheating Measurement of Apollo Shaped Capsule with Boundary Layer Trip in the Free-Piston Shock Tunnel HIEST (AIAA 2014-0434)

    Tanno, H. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2014


    Global Heat Flux Measurement Using Temperature-Sensitive Paint in High-Enthalpy Shock Tunnel HIEST (AIAA 2017-1682)

    Nagayama, Takehiro / Nagai, Hiroki / Tanno, Hideyuki et al. | British Library Conference Proceedings | 2017