Effects of dual jets distance on mixing characteristics and flow path within a cavity in supersonic crossflow

[1]  Hyo-Won Yeom,et al.  Numerical Analysis of a Scramjet Engine with Intake Sidewalls and Cavity Flameholder , 2013 .

[2]  Inyoung Yang,et al.  Effect of Combustor Configuration on Flow and Combustion in a Scramjet Engine , 2013 .

[3]  Christopher P. Goyne,et al.  Experimental Study of Vitiation Effects on Flameholding in a Cavity Flameholder , 2013 .

[4]  A. Oyama,et al.  Feedback Mechanism in Supersonic Laminar Cavity Flows , 2013 .

[5]  K. Kontis,et al.  Plasma actuator: Influence of dielectric surface temperature , 2012 .

[6]  Konstantinos Kontis,et al.  Penetration Characteristics of Air, Carbon Dioxide and Helium Transverse Sonic Jets in Mach 5 Cross Flow , 2012, Sensors.

[7]  E. Erdem,et al.  Experimental Investigation of Transverse Injection Flowfield at Mach 5 and the Influence of Impinging Shock Wave , 2012 .

[8]  Soo-Seok Yang,et al.  Effects of Flameholder Configurations on Combustion in Scramjet Engines , 2012 .

[9]  K. Kontis,et al.  Influence of shock wave propagation on dielectric barrier discharge plasma actuator performance , 2012 .

[10]  Hossein Zare-Behtash,et al.  Effect of primary jet geometry on ejector performance: A cold-flow investigation , 2011 .

[11]  Zheng Wang,et al.  Flow patterns and mixing characteristics of gaseous fuel multiple injections in a non-reacting supersonic combustor , 2011 .

[12]  Jung J. Choi,et al.  Numerical and Experimental Studies of Flame Stability in a Cavity Stabilized Hydrocarbon-Fueled Scramjet , 2011 .

[13]  George N. Barakos,et al.  Review of numerical simulations for high-speed, turbulent cavity flows , 2011 .

[14]  Konstantinos Kontis,et al.  Experimental Studies of Open Cavity Configurations at Transonic Speeds with Flow Control , 2011 .

[15]  Chrisopher O Lada,et al.  Experimental Studies on Transitional and Closed Cavity Configurations Including Flow Control , 2010 .

[16]  K. Kontis,et al.  Experimental investigations of compressible vortex loops , 2008 .

[17]  Russell R. Boyce,et al.  Numerical investigation of transverse jets through multiport injector arrays in supersonic crossflow , 2008 .

[18]  D. Kounadis,et al.  Head-on collision of shock wave induced vortices with solid and perforated walls , 2008 .

[19]  Sang-Hyeon Lee,et al.  Characteristics of Dual Transverse Injection in Scramjet Combustor, Part 1: Mixing , 2006 .

[20]  Campbell D. Carter,et al.  Mixing and combustion studies using cavity-based flameholders in a supersonic flow , 2004 .

[21]  Chrisopher O Lada,et al.  Effect of dimples on glancing shock wave turbulent boundary layer interactions , 2004 .

[22]  J. Schetz,et al.  Flowfield near a Mulitiport Injector Array in a Supersonic Flow , 2000 .

[23]  Kenneth J. Wilson,et al.  Effect of flame-holding cavities on supersonic combustion performance , 1999 .

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

[25]  M. Gruber,et al.  Effects of injector yaw on mixing characteristics of aerodynamic ramp injectors , 1999 .

[26]  J. Schetz,et al.  The flowfield near a multiport injector array in a supersonic flow , 1998 .

[27]  Kenneth J. Wilson,et al.  Experimental Investigation on Dual-Purpose Cavity in Supersonic Reacting Flows , 1998 .

[28]  A. Melling Tracer particles and seeding for particle image velocimetry , 1997 .

[29]  M. R. Gruber,et al.  Mixing and Penetration Studies of Sonic Jets in a Mach 2 Freestream , 1994 .

[30]  S. Obayashi,et al.  Effectiveness of jet location on mixing characteristics inside a cavity in supersonic flow , 2014 .

[31]  Marc Bouchez,et al.  Overview of NATO Background on Scramjet Technology. Chapter 1 , 2006 .

[32]  Campbell D. Carter,et al.  Characteristics of Cavity-Stabilized Flames in a Supersonic Flow , 2005 .

[33]  Yoshiaki Tamura,et al.  Experimental investigation of supersonic internal cavity flows , 1995 .

[34]  Yehuda Salu,et al.  Turbulent diffusion from a quasi-kinematical point of view , 1977 .