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Effect of Inlet Probe Support on Unsteady Aerodynamic Performance of Single-Stage Transonic Compressor

机译：入口探头对单级跨音速压缩机不稳定空气动力学性能的影响

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Rongfei Yang; Yan Xue; Haixu Liu; Chang Liu;
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1. Parametric Study on Aerodynamic Performance of a Single-stage Transonic Axial Compressor with Recirculation-bleeding Channels [J] . Ky-Quang Pham, Quang-Hai Nguyen, Tien-Dung Vuong, International Journal of Fluid Machinery and Systems . 2020,第2期

机译：具有再循环出血通道的单级跨音速轴向压缩机的气动性能的参数研究
2. Investigation of an innovative non-free vortex aerodynamic procedure to design a single-stage transonic compressor [J] . Shahsavari A., Nili-Ahmadabadi M. Proceedings of the Institution of Mechanical Engineers . 2018,第11期

机译：研究设计单级跨音速压缩机的创新性非自由涡流空气动力学程序
3. Constrained Adjoint-Based Aerodynamic Shape Optimization of a Single-stage Transonic Compressor [J] . Benjamin Walther, Siva Nadarajah Journal of turbomachinery . 2013,第2期

机译：单级跨音速压缩机的基于约束的伴随空气动力学形状优化
4. EFFECTS OF A CIRCUMFERENTIAL FEED-BACK CHANNEL ON AERODYNAMIC PERFORMANCE OF A SINGLE-STAGE TRANSONIC AXIAL COMPRESSOR [C] . Cong-Truong Dinh, Sang-Bum Ma, Kwang-Yong Kim ASME turbo expo: turbine technical conference and exposition . 2017

机译：周向反馈通道对单级跨音速轴流压气机气动性能的影响
5. A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor [D] . Heberling, Brian. 2017

机译：自激叶尖流动不稳定性和上游叶片行相互作用对跨音速压缩机性能预测影响的数值分析
6. Aerodynamics of a highly irregular body at transonic speeds—Analysis of STRATOS flight data [O] . Markus Guerster, Ulrich Walter 2011

机译：跨音速下高度不规则物体的空气动力学— STRATOS飞行数据分析
7. Effects of Varying Inlet Guide Vane Pattern on Aerodynamic Mistuning in Transonic Compressors [O] . Daniel Franke, Jonas Foret, Fabian Klausmann, 2020

机译：不同入口导向叶片图案对跨音压缩机空气动力迷雾的影响
8. Investigation of a high-performance axial-flow compressor transonic inlet rotor designed for 37.5 pounds per second per square foot of frontal area I : aerodynamic design and overall performance [R] . Savage, Melvyn, Felix, A Richard 1955

机译：研究高性能轴流式压缩机跨音速入口转子设计为每平方英尺每平方英尺37.5磅每秒I：空气动力学设计和整体性能

Effect of Inlet Probe Support on Unsteady Aerodynamic Performance of Single-Stage Transonic Compressor

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