中国科学院机构知识库网格系统: 检索

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	Simplified Method for Natural Laminar Flow Prediction on Supersonic Highly Swept Wings 期刊论文 OAI收割 AIAA JOURNAL, 2025, 页码: 14 作者: Nie, Han; Liu, Wen; Zhang, Chen-An; Liu, Yang; Guo, Shuai-Qi \| 收藏 \| 浏览/下载：16/0 \| 提交时间：2025/11/03 Mean Aerodynamic Chord Friction Drag Reduction Wing Configurations Laminar to Turbulent Transition Supersonic Aircraft Drag Reduction Boundary Layer Transition Laminar Turbulent Transition Linear Stability Analysis Symbolic Artificial Intelligence
	Experimental Investigation of Shock-Wave-Streamwise-Vortex Interaction 期刊论文 OAI收割 AIAA JOURNAL, 2025, 卷号: 63, 期号: 8, 页码: 3079-3106 作者: Wang, Ziao; Yao, Kai; Chang, Juntao; Yue LJ(岳连捷); Chen, Hao \| 收藏 \| 浏览/下载：14/0 \| 提交时间：2025/09/15 Shock Wave Interaction Vortex Structure Strong Oblique Shock Waves Aerodynamics Fluid Mechanics Aircraft Wing Design Supersonic Wind Tunnels Aircraft Engines Aircraft Components and Structure Flow Conditions
	Development of zone flamelet model for scramjet combustor modeling 会议论文 OAI收割 Xiamen, China, 6-9 March 2017 作者: Yao W(姚卫); Fan XJ(范学军) 收藏 \| 浏览/下载：33/0 \| 提交时间：2018/01/16 Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft
	LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文 OAI收割 Xiamen, China, 6-9 March 2017 作者: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk) 收藏 \| 浏览/下载：46/0 \| 提交时间：2018/01/16 Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow
	Development of zone flamelet modelfor scramjet combustor modeling 会议论文 OAI收割 Xiamen, China, March 6, 2017 - March 9, 2017 作者: Yao W(姚卫); Fan XJ(范学军) \| 收藏 \| 浏览/下载：62/0 \| 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
	A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文 OAI收割 Xiamen, China, 6-9 March 2017 作者: Yao W(姚卫); Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶); Fan XJ(范学军) 收藏 \| 浏览/下载：60/0 \| 提交时间：2018/01/16 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
	Experimental and computational investigation of a full aircraft flutter at transonic speeds 会议论文 OAI收割 Bristol, United kingdom, June 24, 2013 - June 27, 2013 作者: Qian W; Yang GW(杨国伟); Luo JG; Yang R; Zhang GJ \| 收藏 \| 浏览/下载：39/0 \| 提交时间：2018/11/08 Aeroelasticity Aircraft manufacture Airframes Computational fluid dynamics Elastic waves Flutter (aerodynamics) Structural dynamics Supersonic aircraft Transonic aerodynamics Viscous flow Wind stress Wind tunnels Aircraft structure CFD simulations CFD/CSD Computational investigation Flutter boundary predictions Transonic flutter Unsteady aerodynamics Wind tunnel tests
	Numerical analyses of discrete gust response for a flexible aircraft 会议论文 OAI收割 21st AIAA Applied Aerodynamics Conference 2003, Orlando, FL, United states, June 23, 2003 - June 26, 2003 作者: Yang GW(杨国伟); Obayashi S 收藏 \| 浏览/下载：32/0 \| 提交时间：2017/06/01 Direct-coupling method Dynamic equations of motion Flexible aircraft Flexible airplane Freedom of motion One-minus-cosine gust Quasi-steady model Supersonic transport