GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

27-04-2017

Publisher

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

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 1420 : 2011

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 ARP 1210 : 2013	GAS TURBINE ENGINE INTERFACE TEST DATA REDUCTION COMPUTER PROGRAMS
SAE ARP 1257 : 1993	GAS TURBINE ENGINE TRANSIENT PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS
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