热科学学报（英文版）2024，Vol.33Issue(4)：1340-1356,17.DOI:10.1007/s11630-024-1965-5
Aerodynamics of a Tandem-Bladed Axial Compressor Rotor under Circumferential Distortion at Different Rotational Speeds
Aerodynamics of a Tandem-Bladed Axial Compressor Rotor under Circumferential Distortion at Different Rotational Speeds
Amit KUMAR 1Jerry T.JOHN 1A.M.PRADEEP 1R.A.D.AKKERMANS 2Dragan KOZULOVIC3
作者信息
- 1. Department of Aerospace Engineering,Indian Institute of Technology Bombay,Mumbai 400076,India
- 2. Department of Automotive and Aeronautical Engineering,Hamburg University of Applied Sciences,20099 Hamburg,Germany
- 3. Institute of Jet Propulsion,Bundeswehr University Munich,85577 Neubiberg,Germany
- 折叠
摘要
关键词
tandem rotor/circumferential distortion/loss/tip leakage vortex/vortex breakdown/diffusion factor/aerodynamics of compressor bladeKey words
tandem rotor/circumferential distortion/loss/tip leakage vortex/vortex breakdown/diffusion factor/aerodynamics of compressor blade引用本文复制引用
Amit KUMAR,Jerry T.JOHN,A.M.PRADEEP,R.A.D.AKKERMANS,Dragan KOZULOVIC..Aerodynamics of a Tandem-Bladed Axial Compressor Rotor under Circumferential Distortion at Different Rotational Speeds[J].热科学学报（英文版）,2024,33(4):1340-1356,17.
