STABILITY OF PUMPS AND COMPRESSORS
- Author(s):
- Greitzer, Edward M. ( MIT )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1984
- Issue:
- VKI-LS-1984-02-Vol-1
- No.:
- G6/34 92647
- Paper no.:
- N84-25963
- Page(from):
- 1
- Page(to):
- 80
- Pages:
- 80
- Pub. info.:
- National Aeronautics and Space Administration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
National Aeronautics and Space Administration |
The American Society of Mechanical Engineers |
2
Technical Paper
Effects of inlet flow field conditions on the performance of centrifugal compressor diffusers Part 2: Straight-channel diffuser
The American Society of Mechanical Engineers |
8
Technical Paper
Effects of non-axisymmetric tip clearance on axial compressor performance and stability
The American Society of Mechanical Engineers |
3
Technical Paper
Role of blade passage flow structures in axial compressor rotating stall inception
The American Society of Mechanical Engineers |
9
Technical Paper
Dynamic control of rotating stall in axial flow compressors using aeromechanical feedback
The American Society of Mechanical Engineers |
National Aeronautics and Space Administration |
National Aeronautics and Space Adminstration |
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
6
Technical Paper
Effects of inlet flow field conditions on the performance of centrifugal compressor diffusers Part 1: Discrete-passage diffuser
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |