SAE AIR 1419 : 2017

Superseded

View Superseded by

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

Available format(s)

Hardcopy , PDF

Superseded date

23-10-2023

Language(s)

English

Published date

20-11-2017

Publisher

SAE International

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Status	Superseded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	SAE AIR1419D:2023
Supersedes	SAE AIR 1419 : 2013

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 ARP 1210 : 2013	GAS TURBINE ENGINE INTERFACE TEST DATA REDUCTION COMPUTER PROGRAMS
SAE AIR 5686 : 2010	A METHODOLOGY FOR ASSESSING INLET SWIRL DISTORTION
SAE AIR 5826 : 2017	DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES
SAE ARP 1420 : 2002	GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES
SAE AS 755 : 2014	AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION
SAE AIR 5656 : 2016	STATISTICAL STABILITY ASSESSMENT
SAE AS 681 : 2016	GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS
ARP246D: 2012(S2018)	ORIENTATION OF ENGINE AXIS, COORDINATE AND NUMBERING SYSTEMS FOR AIRCRAFT GAS TURBINE ENGINES