Experimental Study of Shock-train/Combustion Coupling and Flame Dynamics in a Heated Supersonic Flow.

[1]  Daniel James Micka,et al.  Combustion stabilization, structure, and spreading in a laboratory dual-mode scramjet combustor , 2010 .

[2]  J. Stevens,et al.  Measured operating characteristics of a rectangular combustor/inlet isolator , 1990 .

[3]  K. Matsuo,et al.  Modified Diffusion Model of Pseudo-Shock Waves Considering Upstream Boundary Layers , 1981 .

[4]  S. Denis,et al.  EXPERIMENTAL STUDY ON TRANSITION BETWEEN RAMJET AND SCRAMJET MODES IN A DUAL-MODE COMBUSTOR , 2003 .

[5]  F. Billig,et al.  Prediction of Precombustion Wall Pressure Distributions in Scramjet Engines , 1973 .

[6]  Yoshiaki Miyazato,et al.  Shock train and pseudo-shock phenomena in internal gas flows , 1999 .

[7]  J. Dutton,et al.  Turbulence phenomena in a multiple normal shock wave/turbulent boundary-layer interaction , 1990 .

[8]  J. Wagner,et al.  Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow , 2009 .

[9]  J. Dutton,et al.  Characteristics of multiple shock wave/turbulent boundary-layer interactions in rectangular ducts , 1990 .

[10]  F. Billig,et al.  Structure of Shock Waves in Cylindrical Ducts , 1973 .

[11]  K. Matsuo,et al.  The Mechanism of Pseudo-Shock Waves , 1974 .

[12]  F. Billig,et al.  Combustion Processes in Supersonic Flow , 1988 .

[13]  Ernest F. Hasselbrink,et al.  Transverse jets and jet flames. Part 1. Scaling laws for strong transverse jets , 2001, Journal of Fluid Mechanics.

[14]  金 羲東.  An experimental study of weak normal shock-wave/turbulent boundary-layer interaction in internal flows , 1992 .

[15]  Youngbin Yoon.  An experimental study of a generic supersonic combustor. , 1994 .

[16]  J. Driscoll,et al.  Stratified Jet Flames in a Heated (1364K) Cross-Flow with Auto-ignition , 2011 .

[17]  Christopher P. Goyne,et al.  Dual-Mode Combustion of Hydrogen in a Mach 5, Continuous-Flow Facility , 2001 .

[18]  J. M. Coulson,et al.  Heat Transfer , 2018, Finite Element Method for Solids and Structures.

[19]  F. Billig.  Research on supersonic combustion , 1992 .

[20]  D. Om,et al.  Multiple transonic shock-wave/turbulent boundary-layer interaction in a circular duct , 1985 .

[21]  R. Bryant.  Planar laser-induced fluorescence images of fuel mixing and the reaction zone in a supersonic combustor , 1998 .

[22]  L. Crocco,et al.  B. One-Dimensional Treatment of Steady Gas Dynamics , 1958 .

[23]  Jens von Wolfersdorf,et al.  Experimental Study on Combustion Mode Transition in a Scramjet with Parallel Injection , 2006 .

[24]  Ronald K. Hanson,et al.  Time evolution and mixing characteristics of hydrogen and ethylene transverse jets in supersonic crossflows , 2006 .

[25]  J. Driscoll,et al.  Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder , 2009 .

[26]  W Merzkirch,et al.  Techniques of Flow Visualization , 1987 .

[27]  Ernest F. Hasselbrink,et al.  Transverse jets and jet flames. Part 2. Velocity and OH field imaging , 2001, Journal of Fluid Mechanics.

[28]  K. Kudo,et al.  Autoignited Combustion Testing in a Water-Cooled Scramjet Combustor , 2004 .

[29]  Christopher P. Goyne,et al.  Experimental Study of a Dual-Mode Scramjet Isolator , 2005 .

[30]  William N. Heltsley,et al.  Combustion Stability Regimes of Hydrogen Jets in Supersonic Crossflow , 2007 .

[31]  K. Hsu,et al.  Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors , 1999 .

[32]  C. Rowley,et al.  On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities , 2002, Journal of Fluid Mechanics.

[33]  O. Dessornes,et al.  Tests of the JAPHAR dual mode ramjet engine , 2005 .

[34]  C. J. Jachimowski,et al.  An analytical study of the hydrogen-air reaction mechanism with application to scramjet combustion , 1988 .

[35]  Ronald K. Hanson,et al.  Diode laser-based detection of combustor instabilities with application to a scramjet engine , 2009 .

[36]  W. Merzkirch,et al.  A simple schlieren interferometer system. , 1965 .

[37]  F. White.  Viscous Fluid Flow , 1974 .

[38]  C. Rasmussen.  An experimental study of flame stability in a directly -fueled wall cavity with a supersonic free stream. , 2006 .

[39]  D. Om,et al.  Transonic shock-wave/turbulent boundary-layer interactions in a circular duct , 1985 .

[40]  J. Rossiter.  Wind tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds , 1964 .

[41]  William H. Heiser,et al.  Hypersonic Airbreathing Propulsion , 1994 .

[42]  W. Merzkirch,et al.  Generalized analysis of shearing interferometers as applied for gas dynamic studies. , 1974, Applied optics.

[43]  G. Settles.  Schlieren and shadowgraph techniques , 2001 .

[44]  Takeshi Kanda,et al.  Dual-Mode Operations in a Scramjet Combustor , 2004 .