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A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun(xfan@imech.ac.cn)
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Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
Blowout limits of supercritical kerosene in supersonic combustors 会议论文
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United states, JUL 14-17, 2013
Authors:  Zhang TC(张泰昌);  Wang J(王晶);  Yuan YM(袁越明);  Li JG(李建国);  Yu G(俞刚);  Fan XJ(范学军);  Zhang TC(张泰昌)
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Visualization of Vaporized Kerosene Combustion in a Supersonic Combustor Using Pulsed Schlieren System 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Atlanta, Georgia, July 30-Augest 1, 2012
Authors:  Yuan YM(袁越明);  Yang M(杨猛);  Zhang TC(张泰昌);  Yu G(俞刚);  Fan XJ(范学军)
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Characteristics of a supersonic model combustor with two-staged injections of supercritical kerosene 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:  Zhang TC(张泰昌);  Yuan YM(袁越明);  Li JG(李建国);  Fan XJ(范学军);  Zhang TC(张泰昌)
View  |  Adobe PDF(636Kb)  |  Favorite  |  View/Download:576/165  |  Submit date:2014/02/24