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Distortion Synthesis/Estimation Techniques
- Aerospace Standard
Published March 21, 2017 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.
This document contains information that is fundamental to the discipline of inlet-engine compatibility and is expected to remain stable for the foreseeable future.
|Aerospace Standard||Inlet/Engine Compatibility - From Model to Full Scale Development|
|Aerospace Standard||A Methodology for Assessing Inlet Swirl Distortion|
|Aerospace Standard||An Assessment of Planar Waves|
Data Sets - Support Documents
|Table 1||Summary of distortion synthesis methods|
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