1–20 von 21 Ergebnissen
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    Component-Based Empirical Model for High-Lift System Noise Prediction

    Y. P. Guo / K. J. Yamamoto / R. W. Stoker | AIAA | 2003

    Jet shock noise at high subsonic flight

    Wat, J. / Yamamoto, K. / Golub, R. | AIAA | 2000

    A study on structure of turbulent premixed flames

    Yamamoto, K. / Achiha, T. / Onuma, Y. | AIAA | 2000

    Supersonic jet noise reduction by a porous single expansion ramp nozzle

    YAMAMOTO, K. / DONELSON, M. / WLEZIEN, R. | AIAA | 1990

    Endurance test of a 35-cm xenon ion thruster

    Hayakawa, Y. / Miyazaki, K. / Kitamura, S. et al. | AIAA | 2000

    Comparison of jet mixing noise predictions with data at high subsonic Mach number

    Wat, J. / Yamamoto, K. / Golub, R. et al. | AIAA | 1999

    Conceptual study of separated core ultra high bypass engine

    SAITO, Y. / ENDOH, M. / SUGAHARA, N. et al. | AIAA | 1992

    Exhaust nozzle research in Japanese HYPR program

    Kishi, K / Kuno, N / Kashiwagi, T et al. | AIAA | 1995

    Large eddy simulation analysis of a 18-lobe convoluted mixer nozzle

    Ooba, Y. / Kodama, H. / Nakamura, Y. et al. | AIAA | 2002

    High Performance DC Arcjet Thruster for 1 kW System Definition

    YOSHIKAWA, T. / ONOE, K. / YAMAMOTO, Y. et al. | AIAA | 1994

    5,000-hour endurance test of a 35-cm xenon ion thruster

    Hayakawa, Y. / Kitamura, S. / Yoshida, H. et al. | AIAA | 2001

    An Evidence-Based Countermeasure for Space Flight:...

    Kulkarni, A / Yamauchi, K / Sundaresan, A et al. | AIAA | 2005

    Analysis of flow in the front-mixing region of hypersonic combined-cycle engine

    Hirai, K. / Kodama, H. / Miyagi, H. et al. | AIAA | 1996

    Balloon-borne experiment with a superconducting solenoidal magnet spectrometer

    Yamamoto, A. / Anraku, K. / Golden, R. et al. | Elsevier | 1993