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An Integrated Total Pressure and Total Temperature Probe for Local Entropy Measurement. Internationa
所属机构名称:中国科学院工程热物理研究所
会议名称:IGTC2011
时间:2011.11.11
成果类型:会议
相关项目:风扇/压气机动叶端区复杂流动结构、非定常激励与失稳调控的基础研究
作者:
Wang, Yongsheng|Lin, Feng|Nie, Chaoqun|
同会议论文项目
风扇/压气机动叶端区复杂流动结构、非定常激励与失稳调控的基础研究
期刊论文 38
会议论文 32
专利 4
同项目会议论文
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An Integrated Total Pressure and Total Temperature Probe for Local Entropy Measurement
Flow Instability Inception Model of Compressors Based on Eigenvalue Theory
Experimental Investigation of Novel Casing Treatment with Bias Flow
Numerical Study on a Kiel Probe Used in Rotor Wake of a High Speed Axial Compressor
Stall Inception Model for Fan/Compressors including the Effect of Three Dimensional Blade Shape
Aerodynamic Analysis of Rotor/Stator Interaction Based on Immersed Boundary Method
Calculation of Flow Instability Inception in High Speed Axial Compressors
The Analysis of Axial Momentum of The Rotor Tip Flows For Axial Compressors With Circumferential Gro
Extensive Experimental Study of Circumferential Single Groove in an Axial Flow Compressor
Investigation of Stability Range Extension Mechanism with Tip Air Injection in a Low-Speed Axial Com
Experimental Investigation of the Influence of Locations of Single Circumferential Groove on a Low-S
Comparison of Stability Range Extension with Micro and Large Air Injection in a Low-Speed Axial Comp
Automatic Efficiency Optimization of an Axial Compressor with Adjustable Inlet Guide Vanes
Total Pressure Averaging in the Wake of a Transonic Axial Compressor
Effects of Casing Groove Depth and Width on the Stability and Efficiency Improvement for a Transonic
The Impact of Groove Location on Tip Clearance Flow and the Stall Margin in an Low-speed Axial Compr
Effect of Novel Casing Treatment on the Suppression of Stall Precursor in a Transonic Compressor
Effect of Advanced Casing Treatment on the Suppression of Precursor of Rotating Stall in transonic C
Experimental investigation of Novel casing treatment with bias flow
Peak Efficiency improvement of a Transonic Fan Rotor by Shaping Circumferential Casing Grooves
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跨音速压气机实验数据分析方法的探索
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离心压气机一维程序开发及验证
The Dynamics of Prestall Process in an Axial Low-speed Compressor with Single Circumferential Casing
Evolution of Pressure Signature Dominated by Unsteady Tip Leakage Flow
Measurements and Visualization of Process from Steady State to Stall in an Axial Compressor with Wat
A Theoretical Model for Flow Instability Inception in Transonic Fan/compressors