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Distortion Synthesis/Estimation Techniques
- Aerospace Standard
- AIR5826
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
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.
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Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 | ||
Table 1 | SUMMARY OF DISTORTION SYNTHESIS METHODS |
Issuing Committee
S-16 Turbine Engine Inlet Flow Distortion Committee
Scope: Committee S-16 develops uniform procedures for adoption by industry. These procedures will permit representation of inletdistortion and evaluation of its effect on propulsion systems' stability and performance.
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