Distortion Synthesis/Estimation Techniques(STABILIZED Mar 2017)

Standard:
Stabilized:
  • 2017-03-21
 
  • CURRENT
Publisher:
  • SAE International
Pages:
15
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:

This document contains information that is fundamental to the discipline of inlet-engine compatibility and is expected to remain stable for the foreseeable future.

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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