SAE AIR 5826 : 2017

SAE AIR 5826 : 2017

DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES

SAE International

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Table of Contents

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

Abstract

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.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee S-16

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