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SAE AIR5826B : 2017

Distortion Synthesis/Estimation Techniques

Standard Details

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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General Information

Status : Stabilized
Standard Type: Main
Document No: SAE AIR5826B : 2017
Document Year: 2017
Pages: 15

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SAE AIR5826B : 2017
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