Performance Impact of Tip Clearance Variation on a Transonic, Low Aspect Ratio, Axial Compressor Stage
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3439
Reference7 articles.
1. The Effect of Tip Clearance on a Swept Transonic Compressor Rotor
2. Compressor Efficiency Variation With Rotor Tip Gap From Vanishing to Large Clearance
3. Effects of Tip Clearance on the Stall Inception Process in an Axial Compressor Rotor
4. The Influence of Tip Clearance Momentum Flux on Stall Inception in a High-Speed Axial Compressor
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1. Effects of the Shock Wave Structure on the Tip Clearance Leakage Flow in Transonic Compressor Rotors;International Journal of Aerospace Engineering;2023-02-20
2. Influence of Fillets on Performance Predictions of a Transonic Axial Compressor Stage at Multiple Tip Clearance Heights;53rd AIAA/SAE/ASEE Joint Propulsion Conference;2017-07-07
3. Improved Predictions of Transonic, Low Aspect Ratio, Axial Compressor Stage Performance and Tip Clearance Effects;54th AIAA Aerospace Sciences Meeting;2016-01-02
4. Two-dimensional modeling of unilateral contact-induced shaft precessional motions in bladed-disk/casing systems;International Journal of Non-Linear Mechanics;2016-01
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