SAE ARP 1420 : 2017
SAE ARP 1420 : 2017
GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES
SAE International
GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES
SAE International
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
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.
Document Type | Standard |
Status | Current |
Publisher | SAE International |
Committee | S-16 |