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A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
Authors:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  Favorite  |  View/Download：176/49  |  Submit date：2022/07/04
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
Authors:  Lu Y(陆阳);  Wang XZ(王新竹);  Li L(李龙);  Cheng D(程迪);  Yuan T(袁涛);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(445Kb)  |  Favorite  |  View/Download：460/95  |  Submit date：2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer  
A Thermal Analysis Method for Fuel-Cooled Combustor Structure based on Heat Flux Measurement 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference., Tours,France, 2012.9.24-28
Authors:  Lu Y(陆阳);  Li L(李龙);  Fan XJ(范学军)
View  |  Adobe PDF(483Kb)  |  Favorite  |  View/Download：1008/372  |  Submit date：2013/02/28
Quasi-1D compressible flow of hydrocarbon fuel 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:  Cheng D(程迪);  Fan XJ(范学军);  Yang M(杨猛);  Cheng D(程迪)
View  |  Adobe PDF(1018Kb)  |  Favorite  |  View/Download：541/153  |  Submit date：2014/02/24