Using forward end-sweep to reduce transonic cantilevered stator losses to improve compressor performance-Reference-Cited by-同舟云学术

Using forward end-sweep to reduce transonic cantilevered stator losses to improve compressor performance

Published:2018-01 Issue:1 Volume:12 Page:293-307
ISSN:1994-2060
Container-title:Engineering Applications of Computational Fluid Mechanics
language:en
Short-container-title:Engineering Applications of Computational Fluid Mechanics

Author:

Lu Hanan¹,Li Qiushi¹²,Pan Tianyu¹²

Affiliation:

1. National Key Laboratory of Science and Technology on Aero-engine Aero-thermodynamics, School of Energy and Power Engineering, Beihang University, Beijing, People’s Republic of China

2. Collaborative Innovation Center of Advanced Aero-Engine, Beihang University, Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation

Aeronautics Power Foundation

Academic Excellence Foundation

Publisher

Informa UK Limited

Subject

Modelling and Simulation,General Computer Science

Link

https://www.tandfonline.com/doi/pdf/10.1080/19942060.2017.1423391

Reference23 articles.

1. Aerodynamics of swept and leaned transonic compressor-rotors

2. Performance Evaluation of Tandem Bladed Centrifugal Compressor

3. The exploitation of three-dimensional flow in turbomachinery design

4. Denton J. D. & Xu L. (2002). The effects of lean and sweep on transonic fan performance (ASME Paper No. GT2002-30327).

5. Effect of Stator Design on Stator Boundary Layer Flow in a Highly Loaded Single-Stage Axial-Flow Low-Speed Compressor

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