SAE AIR5826B

SAE AIR5826B – Distortion Synthesis/Estimation Techniques (Stabilized: Mar 2017)

SAE AIR5826B 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.

Product Details

Published:

03/21/2017

Number of Pages:

15

File Size:

1 file 690 KB

Note:

This product is unavailable in Ukraine Russia Belarus