Aerodynamics of a tandem-bladed axial compressor rotor under circumferential distortion at different rotational speeds

Kumar, Amit; John, Jerry T.; Pradeep, A. M.; Akkermans, Rinie A. D.; Kozulovic, Dragan

doi:10.1007/s11630-024-1965-5

Publisher DOI:	10.1007/s11630-024-1965-5
Title:	Aerodynamics of a tandem-bladed axial compressor rotor under circumferential distortion at different rotational speeds
Language:	English
Authors:	Kumar, Amit John, Jerry T. Pradeep, A. M. Akkermans, Rinie A. D. Kozulovic, Dragan
Keywords:	tandem rotor; circumferential distortion; loss; tip leakage vortex; vortex breakdown; diffusion factor; aerodynamics of compressor blade
Issue Date:	22-Apr-2024
Publisher:	Springer
Journal or Series Name:	Journal of thermal science
Volume:	33
Issue:	4
Startpage:	1340
Endpage:	1356
URI:	http://hdl.handle.net/20.500.12738/15759
ISSN:	1993-033X
Review status:	This version was peer reviewed (peer review)
Institute:	Forschungs- und Transferzentrum Future Air Mobility Fakultät Technik und Informatik Department Fahrzeugtechnik und Flugzeugbau
Type:	Article
Appears in Collections:	Publications without full text