M00014658
New product
INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES
SAE International
In stock
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Availability date: 10/28/2021
1. SCOPE
2. REFERENCES
3. STABILITY MARGIN AND LOSS OF STABILITY
PRESSURE RATIO
4. STABILITY PRESSURE RATIO CORRELATION
5. STABILITY ASSESSMENT
6. PERFORMANCE ASSESSMENT
7. DISTORTION TESTING
8. INTERFACE INSTRUMENTATION AND DATA MANAGEMENT
9. COMPUTATIONAL TECHNIQUES TO EVALUATE
COMPRESSION SYSTEM RESPONSE TO INLET DISTORTION
10. OTHER FORMS OF DISTORTION
11. OTHER OPERABILITY ISSUES
12. SUMMARY
13. NOTES
Specifies many of the significant issues associated with effects of inlet total-pressure distortion on turbine-engine performance and stability.
Published | |
Document Type | Standard |
Status | Current |
Publisher | SAE International |
Pages | |
ISBN | |
Committee | S-16 |