Performance Estimation Method for Nonuniform Tip Clearance Cases-Reference-Cited by-同舟云学术

Performance Estimation Method for Nonuniform Tip Clearance Cases

Published:2018-11 Issue:6 Volume:34 Page:1355-1363
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Chen Yingxiu¹,Hou Anping¹,Wang Weiwei¹,Zhang Mingming²

Affiliation:

1. Beihang University, 100191 Beijing, People’s Republic of China

2. Beijing University of Technology, 100124 Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B36442

Reference28 articles.

1. High-Pressure-Turbine Clearance Control Systems: Current Practices and Future Directions

2. SteenkenW. G.WilliamsJ. G.YuhasA. J.WalshK. R. “Factors Affecting Inlet-Engine Compatibility During Aircraft Departures at High Angle of Attack for an F/A-18A Aircraft,” NASA TM-1999-206572, 1999.

3. Analysis and solution of the rotor instability problem in the advanced model TF30 P111+ engine

4. Effects of Nonaxisymmetric Tip Clearance on Axial Compressor Performance and Stability

5. Unsteady Flow and Whirl-Inducing Forces in Axial-Flow Compressors: Part I—Experiment

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