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Axial Compressor Stall, Circumferential Groove Casing Treatment, and the Tip-Clearance Momentum Flux
- Source :
- Journal of Propulsion and Power. 34:146-152
- Publication Year :
- 2018
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2018.
-
Abstract
- The stall margin and pressure ratio of an axial compressor can both be increased with the use of circumferential groove casing treatments over the rotor. Performance and stall point measurements we...
- Subjects :
- Compressor stall
Overall pressure ratio
020301 aerospace & aeronautics
Hardware_MEMORYSTRUCTURES
Materials science
business.industry
Mechanical Engineering
Aerospace Engineering
Stall (fluid mechanics)
02 engineering and technology
Mechanics
Structural engineering
Static pressure
01 natural sciences
010305 fluids & plasmas
Tip clearance
Fuel Technology
Axial compressor
0203 mechanical engineering
Space and Planetary Science
0103 physical sciences
Mass flow rate
business
Casing
Subjects
Details
- ISSN :
- 15333876 and 07484658
- Volume :
- 34
- Database :
- OpenAIRE
- Journal :
- Journal of Propulsion and Power
- Accession number :
- edsair.doi...........45517e8455d032f040465892efa87aac