SAE AIR1419C
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES
Hardcopy , PDF
23-10-2023
English
20-11-2017
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.
Committee |
S-16
|
DocumentType |
Revision
|
Pages |
226
|
ProductNote |
This standard lso referes to 680286,740824
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
SAE AIR 5396A: 2015 | CHARACTERIZATIONS OF AIRCRAFT ICING CONDITIONS |
SAE AIR 5866 : 2008 | AN ASSESSMENT OF PLANAR WAVES |
SAE AIR 5687 : 2016 | INLET/ENGINE COMPATIBILITY - FROM MODEL TO FULL SCALE DEVELOPMENT |
SAE ARP1210D | GAS TURBINE ENGINE INTERFACE TEST DATA REDUCTION COMPUTER PROGRAMS |
SAE AIR 5826 : 2017 | DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES |
SAE ARP 1420 : 2002 | GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES |
SAE AS755E | AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION |
SAE AIR 5656 : 2016 | STATISTICAL STABILITY ASSESSMENT |
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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