Effects of Rotor-Bleeding Airflow on Aerodynamic and Structural Performances of a Single-Stage Transonic Axial Compressor

Author:

Dinh Cong-TruongORCID,Vu Dinh-Quy,Kim Kwang-Yong

Funder

National Foundation for Science and Technology Development

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Reference27 articles.

1. Andrew JY, Ronald JR (1992) Effects of bleed air extraction on thrust level of the F404-GE-400 turbofan engine. NASA TM-104247, the AIAA 28th joint propulsion conference, Nashville, Tennessee

2. Hathaway MD (2002) Self-recirculating casing treatment concept for enhanced compressor performance. In: Proceedings of the ASME turbo expo 2002, Amsterdam, Netherlands, GT2002-30368

3. Wellborn SR, Michael LK (2002) Bleed flow interactions with an axial-flow compressor power-stream. In: 38th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Indianapolis, Indiana, USA, AIAA Paper 2002-4057

4. Ress RA, Carmel J., Hansen JL (2002) Compressor endwall bleed system. U.S. Patent 6,428,271 B1

5. Gomes RA, Schwarz C, Pfitzner M (2006) Experimental investigation of a generic compressor bleed system. In: Proceedings of the ASME Turbo Expo 2006, Barcelona, Spain, GT2006-90458

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