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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 :

    01.01.2018


    Format / Umfang :

    7 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



    Heat Flux Measurement of Apollo Capsule Model at High Stagnation Pressure in Shock Tunnel HIEST

    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



    Boundary Layer Transition and Trip Effectiveness on an Apollo Capsule in the JAXA High Enthalpy Shock Tunnel (HIEST) Facility (AIAA 2015-0209)

    Kirk, Lindsay / Lillard, Randolph P. / Olejniczak, Joseph et al. | British Library Conference Proceedings | 2015