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Distortion Synthesis/Estimation Techniques
- Aerospace Standard
Published October 13, 2016 by SAE International in United States
Downloadable datasets availableAnnotation ability available
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.
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.
|Aerospace Standard||Distortion Synthesis/Estimation Techniques|
|Technical Paper||Simulation of the Effect of Spatial Fuel Distribution Using a Linear-Eddy Model|
Data Sets - Support Documents
|Table 1||Summary of distortion synthesis methods|
S-16 Turbine Engine Inlet Flow Distortion Committee
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