1–15 von 15 Ergebnissen
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    Detection of Driver Gas Contamination in the T5 Hypervelocity Shock Tunnel

    Sudani, N. / Hornung, H. G. / AIAA | British Library Conference Proceedings | 1997

    Flow Angularity Measurement of JAXA 2m x 2m Transonic Wind Tunnel

    Ueno, M. / Sudani, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

    Numerical Simulation of Flowfields of the NAL Two-Dimensional Transonic Wind Tunnel

    Matsuno, K. / Satofuka, N. / Sudani, N. et al. | British Library Online Contents | 1996

    Wall and Support Interference Corrections of NASA Common Research Model Wind Tunnel Tests in JAXA

    Kohzai, M. / Ueno, M. / Koga, S. et al. | British Library Conference Proceedings | 2013

    Cell Structure on Circular Cylinders near the Critical Reynolds Number

    Yoshinaga, T. / Sato, M. / Tate, A. et al. | British Library Conference Proceedings | 1998

    Analysis of NASA Common Research Model Dynamic Data in JAXA Wind Tunnel Tests

    Koga, S. / Kohzai, M. / Ueno, M. et al. | British Library Conference Proceedings | 2013

    Calibration of the Test Section Mach Number in the JAXA 2m x 2m Transonic Wind Tunnel

    Kohzai, M. / Ueno, M. / Shiohara, T. et al. | British Library Conference Proceedings | 2008

    80% Scaled NASA Common Research Model Wind Tunnel Test of JAXA at Relatively Low Reynolds Number

    Ueno, M. / Kohzai, T. / Koga, S. et al. | British Library Conference Proceedings | 2013

    Three-Dimensional Effects on Shock Wave Reflections in Steady Flows

    Sudani, N. / Sato, M. / Watanabe, M. et al. | British Library Conference Proceedings | 1999

    Numerical Simulation of Flowfields of the NAL Two-Dimensional Transonic Wind Tunnel

    Matsuno, K. / Satofuka, N. / Sudani, N. et al. | British Library Conference Proceedings | 1996