IMECH-IR

浏览/检索结果: 共3条,第1-3条 帮助

限定条件                    
已选(0)清除 条数/页:   排序方式:
A novel method of cooling channel optimization for active-cooled structure using the calculus of variations 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者:  Li X(李轩);  Lu Y(陆阳);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(705Kb)  |  收藏  |  浏览/下载:176/60  |  提交时间:2020/11/20
Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载:258/87  |  提交时间:2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载:272/81  |  提交时间:2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion