SAE AIR1419C
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines
Hardcopy , PDF
23-10-2023
English
20-11-2017
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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.
| DocumentType |
Standard
|
| Pages |
226
|
| ProductNote |
This standard lso referes to 680286,740824
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
This document addresses many of the significant issues associated with effects of inlet total-pressure distortion on turbine-engine performance and stability. It provides a review of the development of techniques used to assess engine stability margins in the presence of inlet total-pressure distortion. Specific performance and stability issues that are covered by this document include total-pressure recovery and turbulence effects and steady and dynamic inlet total-pressure distortion.
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