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    Titel :

    Computations of Opposing Jet from Vertical Landing Rocket Vehicle



    Kongress:

    25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA



    Erscheinungsdatum :

    01.01.2006


    Format / Umfang :

    AIAA Paper 2006-3329


    Anmerkungen:

    Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    PIV Measurement of Opposing Jet Flow on Vertical Landing Rocket

    H. Kato / S. Watanabe / T. Hashimoto et al. | NTIS | 2005


    Aerodynamic Effects of Opposing Nozzle Jet on Reusable Vertical Landing Rocket

    Akita, D. | British Library Conference Proceedings | 2002


    Aerodynamic design considerations in vertical landing rocket vehicle

    Nonaka, Satoshi / Ogawa, Hiroyuki / Inatani, Yoshifumi | AIAA | 2001


    Throttling Dynamic Response of LH2 Rocket Engine for Vertical Landing Rocket Vehicle

    Naruo, Y. / Inatani, Y. / Morita, Y. et al. | British Library Conference Proceedings | 1997