Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Scramjet Engine Test at Mach 6 Flight Condition



    Kongress:

    33rd, Joint propulsion conference ; 1997 ; Seattle: WA


    Erscheinungsdatum :

    01.01.1997


    Format / Umfang :

    ALL


    Anmerkungen:

    Nos 97-2914 to 97-3388 with gaps


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Scramjet engine test at the Mach 6 flight condition

    Sato, Shigeru / Izumikawa, Muneo / Tomioka, Sadatake et al. | AIAA | 1997


    Ignition Transient Phenomena in a Scramjet Engine at Mach 12 Flight Condition

    Kodera, Masatoshi / Yang, Vigor / Takahashi, Masahiro et al. | AIAA | 2007


    Performance Characteristics of a Scramjet Engine at Mach 10 to 15 Flight Condition

    Takahashi, Masahiro / Sunami, Tetsuji / Tanno, Hideyuki et al. | AIAA | 2005


    Evaluation of Heat-flux on Scramjet Engine Wall in Mach 6 Flight Condition

    Ueda, Shuichi / Takegoshi, Masao / Kouchi, Toshinori et al. | AIAA | 2006


    Scramjet Engine Flowpath Development for the Hyper-X Mach 10 Flight Test

    Rogers, R. C. / Shih, A. T. / Hass, N. E. | NTRS | 2005