Standard

SAE AIR5826A

Oct 2016 Withdrawn

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Language English

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Abstract

This document provides 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. The methods have been categorized based on the underlying mathematical representation of the aerophysics. Further, the use of maximum value statistics, which has been used to further improve the results where short-duration time records have been employed, is discussed.

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Standard from SAE International
Published: October 13 2016
Withdrawn: March 21 2017
Document type: IS
Pages
ISBN:

Publisher: SAE International
Distributor: SAE International

Product Relations

Replaced by: SAE AIR5826B
Replaces: SAE AIR5826

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Version history History (2)

SAE AIR5826A

SAE AIR5826

Abstract

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