Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Global Heat Transfer Measurement in a Hypersonic Shock Tunnel Using Temperature-Sensitive Paint


    Contributors:
    Nakakita, K. (author) / Osafune, T. (author) / Asai, K. (author) / AIAA

    Conference:

    41st, Aerospace sciences meeting ; 2003 ; Reno, NV



    Publication date :

    2003-01-01


    Size :

    ALL


    Remarks:

    Paper nos AIAA-2003-0001 to AIAA-2003-1359 with gaps


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Global Heat Transfer Measurement in a Hypersonic Shock Tunnel Using Temperature-Sensitive Paint

    Nakakita, Kazuyuki / Osafune, Tatsuya / Asai, Keisuke | AIAA | 2003


    Pressure sensitive paint measurement in a hypersonic shock tunnel

    Nakakita, Kazuyuki / Yamazaki, Takashi / Asai, Keisuke et al. | AIAA | 2000


    Global Heat Flux Measurement Using Temperature-Sensitive Paint in High-Enthalpy Shock Tunnel HIEST

    Nagayama, Takehiro / Nagai, Hiroki / Tanno, Hideyuki et al. | AIAA | 2017



    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