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Distortion Synthesis/Estimation Techniques
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STANDARD published on 1.3.2017
Designation standards: SAE AIR5826B
Publication date standards: 1.3.2017
SKU: NS-678206
Country: American technical standard
Category: Technical standards SAE
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.
SUBJECT TAXONOMY: Simulation and modeling, Engines, Gas turbines
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard
Stabilized: Mar 2017
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