Unified treatment of flow instabilities of turbomachines

Journal of Propulsion and Power

Volumn 17, Issue 3, 2001, Pages 636-643

  Tsujimoto, Yoshinobu ^a   Kamijo, Kenjiro ^b   Brennen, Christopher E ^c  

^a OSAKA UNIVERSITY   (Japan)

^b TOHOKU UNIVERSITY   (Japan)

^c California Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CAVITATION; IMPELLERS; VISCOUS FLOW;

CAVITATION SURGE; IMPELLER BLADES;

TURBOMACHINE BLADES;

EID: 0035332673     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5790     Document Type: Article

References (16)

1. Surge and rotating stall in axial flow compressors part 1 - Theoretical compression system model
2. Surge and rotating stall in axial flow compressor: Part 2 - Experimental results and comparison with theory
3. A simple model for compressor stall cell propagation
4. A theory of rotating stall of multistage axial compressors: Part I - Small disturbances
5. A theory of post-stall transients in axial compression systems: Part II - Application
6. A metod for assesing effects of inlet flow distortion on compressor stability
7. A theoretical analysis of rotating cavitation in inducers
8. The dynamic transfer function for a cavitating inducer
9. Experiments on the dynamic behavior of cavitating pumps
10. The bubbly flow model for the dynamic characteristics of cavitating pump
11. A visual observation of cavitating inducers
12. Hydraulic and mechanical performance of LE-7 LOX pump inducer
13. Experimental study on rotating cavitation of rocket propellant pump inducers
14. Observations of cavitation and flow patterns in an axial flow pump at low flow rate