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SAE ARP 1420 : 2017

SAE ARP 1420 : 2017

GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES

SAE International

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Table of Contents

1. SCOPE
2. REFERENCES
3. PURPOSE
4. PROVISIONS
5. DISTORTION DESCRIPTOR FORMAT AND USAGE
6. STABILITY AND PERFORMANCE ASSESSMENT
7. TESTING
8. INTERFACE INSTRUMENTATION AND DATA MANAGEMENT
APPENDIX A - DISTORTION ELEMENT CALCULATIONS AND STABILITY
             PRESSURE RATIO LOSS CORRELATION

Abstract

Concerns only to the effects of inlet total-pressure distortion. The guidelines can be used as necessary to create a development method to minimize the risk of inlet/engine compatibility problems.

General Product Information

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

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