Unsteady behavior of oblique shock train and boundary layer interactions
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[1] Chengpeng Wang,et al. Experimental characteristics of oblique shock train upstream propagation , 2017 .
[2] Zhenguo Wang,et al. Experimental study on the flow separation and self-excited oscillation phenomenon in a rectangular duct , 2017 .
[3] Hossein Zare-Behtash,et al. Pseudo-shock waves and their interactions in high-speed intakes , 2016 .
[4] J. Driscoll,et al. Response of a shock train to downstream back pressure forcing , 2016 .
[5] P. Bruce,et al. Shock Wave Boundary Layer Interaction Unsteadiness: The Effects of Configuration and Strength , 2016 .
[6] Datta V. Gaitonde,et al. Progress in shock wave/boundary layer interactions , 2013 .
[7] Noel T. Clemens,et al. Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions , 2014 .
[8] Jinglei Xu,et al. Principal Parameters in Flow Separation Patterns of Over-Expanded Single Expansion RAMP Nozzle , 2014 .
[9] Xinyu Zhang,et al. Interaction of Isentropic Compression Waves with a Bow Shock , 2013 .
[10] J. Qin,et al. Novel Oscillatory Patterns of Hypersonic Inlet Buzz , 2012 .
[11] He-xia Huang,et al. Behavior of shock trains in a hypersonic inlet/isolator model with complex background waves , 2012 .
[12] Liu Weidong,et al. Experimental investigation of the micro-ramp based shock wave and turbulent boundary layer interaction control , 2012 .
[13] C. Hirsch,et al. Experimental and Numerical Study of Oscillating Transonic Shock Waves in Ducts , 2011 .
[14] Holger Babinsky,et al. An experimental study of transonic shock/boundary layer interactions subject to downstream pressure perturbations , 2010 .
[15] H. Tan,et al. Oscillatory Flows of Rectangular Hypersonic Inlet Unstart Caused by Downstream Mass-Flow Choking , 2009 .
[16] H. Babinsky,et al. Unsteady shock wave dynamics , 2008, Journal of Fluid Mechanics.
[17] Arnaud Galli,et al. Control of forced shock-wave oscillations and separated boundary layer interaction , 2005 .
[18] Reynald Bur,et al. Experimental and numerical study of forced shock-wave oscillations in a transonic channel , 2006 .
[19] K. Matsuo,et al. Mechanism of Shock Wave Oscillation in Transonic Diffusers , 2003 .
[20] R. Bur,et al. Modeling of Controlled Shock-Wave/Boundary-Layer Interactions in Transonic Channel Flow , 2001 .
[21] Yoshiaki Miyazato,et al. Shock train and pseudo-shock phenomena in internal gas flows , 1999 .
[22] Jean Delery,et al. Study of Passive Control in a Transonic Shock Wave/Boundary-Layer Interaction , 1998 .
[23] E. T. Curran,et al. Fluid Phenomena in Scramjet Combustion Systems , 1996 .
[24] J. Dutton,et al. Characteristics of multiple shock wave/turbulent boundary-layer interactions in rectangular ducts , 1990 .
[25] D. Om,et al. Multiple transonic shock-wave/turbulent boundary-layer interaction in a circular duct , 1985 .
[26] T. J. Bogar,et al. Forced Oscillation Experiments in Supercritical Dif f user Flows , 1984 .
[27] T. Bogar,et al. Characteristic frequencies of transonic diffuser flow oscillations , 1983 .
[28] T. Bogar,et al. Response of a Supersonic Inlet to Downstream Perturbations , 1983 .
[29] M. Sajben,et al. Effects of Initial Boundary-Layer Thickness on Transonic Diffuser Flows , 1981 .
[30] J. C. Kroutil,et al. Shock-Wave Oscillations in a Transonic Diffuser Flow , 1979 .
[31] F. Billig,et al. Structure of Shock Waves in Cylindrical Ducts , 1973 .
[32] J. Swithenbank. Hypersonic air-breathing propulsion , 1967 .