Combined Pressure and Temperature Distortion Effects on Internal Flow of a Turbofan Engine
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.57927
Reference13 articles.
Cited by 11 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Stall and stability enhancement mechanisms of transonic compressor with inlet total temperature distortion;Physics of Fluids;2023-12-01
2. The Influences of Combined Distortions on Fan Performance;Advances in Turbomachinery;2023-05-31
3. Numerical investigations of mass-flux redistribution and performance prediction model on coupling effects of total pressure distortion-low Reynolds number in axial compressor;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2022-11-22
4. A new distortion evaluation method based on geometric association for arbitrary cross-sectional shape of inlet;Aerospace Science and Technology;2022-09
5. Non-intrusive flow diagnostics for unsteady inlet flow distortion measurements in novel aircraft architectures;Progress in Aerospace Sciences;2022-04
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