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SAE AIR 1419 : 2017

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SAE AIR 1419 : 2017

INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES

SAE International

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Table of Contents

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

Abstract

Specifies many of the significant issues associated with effects of inlet total-pressure distortion on turbine-engine performance and stability.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee S-16