Distortion Synthesis/Estimation Techniques

Standard:
Revised:
  • 2016-10-13
 
  • HISTORICAL Access the latest revision: AIR5826B
Publisher:
  • SAE International
Pages:
14
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.

Rationale:

The purposes of this revision were to make some editorial corrections, add the Rationale, and otherwise bring its dated format into conformity with the more recent SAE standards.

History:
Standard Published Revision Status
AIR5826B 2017-03-21 Latest Stabilized
2016-10-13 Historical Revised
2011-07-20 Historical Reaffirmed
AKA:
  • SAE AIR 5826
Sector:
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