论文部分内容阅读
Investigation on the Performance of Highly Loaded Transonic Rotor with Forward Sweep
【机 构】
:
Institute of Engineering Thermophysics, Chinese Academy of Sciences; University of Chinese Academy o
【出 处】
:
第六届亚洲推进与动力国际会议
【发表日期】
:
2012年9期
其他文献
Study on Design and Combustion Characteristics for a Uni-Injector using Gas Methane/Lox as propellan
Prediction of First Rotating Stage for Contra-rotating Compressor under Different Rotating Speed Rat
Spray Characteristics under Various Injection Conditions for a Nonimpinging-type Injector Utilized i
Investigation on corner separation control in a compressor cascade using plasma aerodynamic actuatio
The heat transfer correlation of hydrocarbon fuel in laminar and transitional flow regions under sup
Electric heating tube is an often used method to study the heat transfer correlation of supercritical hydrocarbon.Many researchers have obtained different correlations in turbulent flow region with di
Research on the Effect of the Radius of Forebody Leading Edge on the Characteristic of SWBLI on Hype
Shock wave/boundary layer interaction (SWBLI) on hypersonic inlet external compression surface has remarkably influence on the inlet performance,and the characteristic of SWBLI on the forebody of airc