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SAE AIR 5826 : 2017

Current
Current

The latest, up-to-date edition.

DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

03-21-2017

Publisher

SAE International

1 SCOPE
2 REFERENCES
3 BACKGROUND
4 REVIEW OF CURRENT STATUS
5 RECOMMENDATIONS
6 NOTES

Gives a review of published methods that have been used to provide estimates of the levels of distortion and/or the concomitant loss of stability pressure ratio that can occur when the recommended full complement of aerodynamic interface plane high-response instrumentation is not used when obtaining inlet data.

Committee
S-16
DocumentType
Standard
Pages
15
ProductNote
This version is now stabilized.
PublisherName
SAE International
Status
Current
Supersedes

SAE AIR 5686 : 2010 A METHODOLOGY FOR ASSESSING INLET SWIRL DISTORTION
MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
SAE AIR 1419 : 2017 INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES

SAE ARP 1420 : 2002 GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES

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Hardcopy - English
PDF - English
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