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许登科 ( 副研究员 ) 赞
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[11] .Stall Inception Prediction of Axial Compressors with Radial Inlet Distortions:Aerospace Science and Technology
[12] .Effect of Rotor Axial Blade Loading Distribution on Compressor Stability:Aerospace Science and Technology
[13] .Effect of Rotor Blade Loading Distribution on Flow Stability of Transonic Compressor:Aerospace Science and Technology
[14] .Theoretical and Experimental Investigation on the Stall Inception of Low-Speed Axial Compressors with Swept Rotor Blades:Aerospace Science and Technology
[15] .Flow Stability Analysis on Low-Speed Compressor with Swept Rotor Blades under Radial Inlet Distortions:Aerospace Science and Technology
[16] .Bi-Global Stability Analysis on Flow Separation of Two-Dimensional Compressor Cascade:Aerospace Science and Technology
[17] .Analysis of Flow Characteristics and Flow Stability on an Axial Compressor with Inlet Temperature Ramp Distortion:Aerospace Science and Technology
[18] .A Modified Small Perturbation Stability Prediction Model for Axial Compressors with Circumferential Inlet Distortion:Aerospace Science and Technology
[19] .Effect of Fore/Aft-Loaded Rotor on Compressor Stability under Inlet Circumferential Distortion:Chinese Journal of Aeronautics
[20] .Sensitivity Analysis for Stall Inception of Transonic Rotor Based on Meridional Flow:Chinese Journal of Aeronautics

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