Distortion Synthesis/Estimation Techniques

Product Code: AIR5826

Date Published: 2004-06-09
Date Reaffirmed: July 2011

Issuing Committee:

S-16 Turbine Engine Inlet Flow Distortion Committee

Scope

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.

Product Status: In Stock

File Size: 446K

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Current & Historical versions of this standard
Standard	Date published	?Status
AIR5826	2004-06-09	Reaffirmed

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Distortion Synthesis/Estimation Techniques

Issuing Committee:

Scope

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