SAE ARP1420C
Current
The latest, up-to-date edition.
GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES
Hardcopy , PDF
English
27-04-2017
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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
The turbine-engine inlet flow distortion methodology addressed in this document applies only to the effects of inlet total-pressure distortion.
| Committee |
S-16
|
| DocumentType |
Standard
|
| Pages |
25
|
| ProductNote |
THIS STANDARD IS NOW STABILIZED
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| SAE ARP 755 : 2014 | AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION AND NOMENCLATURE |
| SAE AIR 1419 : 2013 | INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES |
| SAE ARP1210D | GAS TURBINE ENGINE INTERFACE TEST DATA REDUCTION COMPUTER PROGRAMS |
| SAE ARP 1257 : 1993 | GAS TURBINE ENGINE TRANSIENT PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS |
| SAE AS681K | GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS |
| SAE ARP246D | ORIENTATION OF ENGINE AXIS, COORDINATE AND NUMBERING SYSTEMS FOR AIRCRAFT GAS TURBINE ENGINES |
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