SAE ARP 1420 : 2002
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES
Available format(s)
Hardcopy , PDF
Superseded date
14-05-2017
Superseded by
Language(s)
English
Published date
01-01-2002
Publisher
DocumentType |
Standard
|
Pages |
24
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy |
SAE AIR 4869 : 2015 | DESIGN CONSIDERATIONS FOR ENCLOSED TURBOFAN/TURBOJET ENGINE TEST CELLS |
JSGS-87231 Revision A:1995 | ENGINES, AIRCRAFT, TURBINE |
SAE AIR 1419 : 2017 | INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES |
SAE AS681K | GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS |
SAE ARP 1257 : 1993 | GAS TURBINE ENGINE TRANSIENT PERFORMANCE PRESENTATION FOR DIGITAL COMPUTER PROGRAMS |
MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
SAE AIR 5867 : 2017 | ASSESSMENT OF THE INLET/ENGINE TOTAL TEMPERATURE DISTORTION PROBLEM |
JSSG-2001 Revision B:2004 | Air Vehicle |
SAE AIR 5686 : 2010 | A METHODOLOGY FOR ASSESSING INLET SWIRL DISTORTION |
SAE AIR 1703 : 2012 | IN-FLIGHT THRUST DETERMINATION |
SAE AIR 5687 : 2016 | INLET/ENGINE COMPATIBILITY - FROM MODEL TO FULL SCALE DEVELOPMENT |
SAE AIR 5826 : 2017 | DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES |
SAE AIR 5656 : 2016 | STATISTICAL STABILITY ASSESSMENT |
SAE AIR1419D:2023 | Inlet Total-Pressure Distortion Considerations for Gas-Turbine Engines |
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