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SAE AIR5826 Rev B

Distortion Synthesis/Estimation Techniques
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SAE AIR5826 Rev B

Distortion Synthesis/Estimation Techniques

PUBLISH DATE 2017
PAGES 15
SAE AIR5826 Rev B
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.
SDO SAE: SAE International
Document Number AIR5826
Publication Date March 21, 2017
Language en - English
Page Count 15
Revision Level B
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