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    Computational Analysis of Characteristics of Mach Wave Sources in Supersonic Free-Jets

    Nonomura, T. / Fujii, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009

    Mach Number and Temperature Effects on Mach Wave Emission from Supersonic Jets

    Nonomura, T. / Fujii, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

    Detailed Analysis of Flat Plate Pressure Peaks Created by Supersonic Jet Impingements

    Goto, Y. / McIlroy, K. / Nonomura, T. et al. | British Library Conference Proceedings | 2009

    Comparative Study of Co-flow and Counter Blowing DBD Plasma Actuators for Separated Flow over an Airfoil

    Sekimoto, S. / Asada, K. / Anyoji, M. et al. | British Library Conference Proceedings | 2012

    EFFECTS OF SHEAR-LAYER CHARACTERISTIC ON THE FEEDBACK-LOOP MECHANISM IN SUPERSONIC OPEN CAVITY FLOWS

    Li, W. / Nonomura, T. / Fujii, K. et al. | British Library Conference Proceedings | 2011

    ACOUSTIC WAVES FROM A SUPERSONIC JET IMPINGING ON AN INCLINED FLAT PLATE

    Nonomura, T. / Goto, Y. / Fujii, K. et al. | British Library Conference Proceedings | 2010

    Numerical Analysis of the Aerodynamic Characteristics of SSTO Configurations with an Aerospike Nozzle

    Tsukada, H. / Fujimoto, K. / Nonomura, T. et al. | British Library Conference Proceedings | 2005

    MACH NUMBER EFFECTS ON VORTEX BREAKDOWN IN SUBSONIC FLOW OVER A DELTA WING

    Fukumoto, H. / Ishikawa, Y. / Nonomura, T. et al. | British Library Conference Proceedings | 2011

    Computational Analysis of Mach Number Effects on Edgetone

    Nonomura, T. / Muranaka, H. / Fujii, K. et al. | British Library Conference Proceedings | 2006

    Massive Parametric Study by LES on Separated-flow Control around Airfoil using DBD Plasma Actuator at Reynolds Number 63,000

    Sato, M. / Okada, K. / Nonomura, T. et al. | British Library Conference Proceedings | 2013

    Increasing Order of Accuracy of Weighted Compact Non-Linear Scheme AIAA Paper

    Nonomura, T. / Iizuka, N. / Fujii, K. et al. | British Library Conference Proceedings | 2007

    Experimental Study of a Nano-second Pulse Plasma Actuator for Low Reynolds Number Flow Control (AIAA 2014-0767)

    Sekimoto, S. / Sulaiman, T. / Anyoji, M. et al. | British Library Conference Proceedings | 2014

    Effect of Wing Planform on Aerodynamic Characteristics at Low Reynolds Numbers using a Low Density Wind Tunnel

    Anyoji, M. / Liu, T. / Nonomura, T. et al. | British Library Conference Proceedings | 2013

    EXPERIMENTAL STUDY OF EFFECTS OF FREQUENCY FOR BURST WAVE ON DBD PLASMA ACTUATOR FOR SEPARATION CONTROL

    Sekimoto, S. / Asada, K. / Usami, T. et al. | British Library Conference Proceedings | 2011

    Effect of Burst Frequency and Reynolds Number on Flow Control Authority of DBD Plasma Actuator on NACA0012 Airfoil (AIAA 2014-1245)

    Sulaiman, T. / Aono, H. / Sekimoto, S. et al. | British Library Conference Proceedings | 2014

    FLOW FIELD DATA MINING OF PARETO-OPTIMAL AIRFOILS USING PROPER ORTHOGONAL DECOMPOSITION

    Oyama, A. / Verburg, P. / Nonomura, T. et al. | British Library Conference Proceedings | 2010