DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

21-03-2017

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 5826 : 2004

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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SAE AIR 5826 : 2017

DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES

Table of Contents

Abstract

General Product Information

Standards Referenced By This Book

Standards Referencing This Book

Category

Subcategory