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Theory of Compressor Stability Enhancement Using Novel Casing Treatment, Part II: Experiment
- Source :
- Journal of Propulsion and Power. 30:1236-1247
- Publication Year :
- 2014
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2014.
-
Abstract
- A stall precursor-suppressed casing treatment is designed to enhance stall margin for both subsonic and transonic compressors. It is noted that the open area ratio of the stall precursor-suppressed casing treatment is only 4–10%, far smaller than conventional casing treatments, with over 50% open area ratio. The effect of the novel casing treatment on the stall margin and efficiency of compressors has been investigated experimentally. The results show that the stall precursor-suppressed casing treatment can improve the stall margin by about 8–18% without significantly decreasing the efficiency of the related fan/compressors. Meanwhile, the present investigation has also attempted to reveal the mechanism of stall margin improvement with such casing treatment. It is found that the stall precursor-suppressed casing treatment will delay the nonlinear development of the stall process by suppressing the propagation of the stall precursor waves, as compared with the evolution of the precursors without casing tre...
- Subjects :
- Compressor stall
Hardware_MEMORYSTRUCTURES
Materials science
business.industry
Mechanical Engineering
Aerospace Engineering
Stall (fluid mechanics)
Structural engineering
Static pressure
ComputerSystemsOrganization_PROCESSORARCHITECTURES
enzymes and coenzymes (carbohydrates)
Fuel Technology
Axial compressor
Space and Planetary Science
Mass flow rate
business
Casing
Transonic
Gas compressor
Subjects
Details
- ISSN :
- 15333876 and 07484658
- Volume :
- 30
- Database :
- OpenAIRE
- Journal :
- Journal of Propulsion and Power
- Accession number :
- edsair.doi...........7fe09ce2e393331a67d16b32f8b4faae
- Full Text :
- https://doi.org/10.2514/1.b34901