1951476

SAE ARP1420C

Gas Turbine Engine Inlet Flow Distortion Guidelines (Stabilized: Apr 2017)

standard by SAE International , 04/27/2017

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The turbine-engine inlet flow distortion methodology addressed in this document applies only to the effects of inlet total-pressure distortion. Practices employed to quantify these effects continue to develop and, therefore, periodic updates are anticipated. The effects of other forms of distortion on flow stability and performance, and of any distortion on aeroelastic stability are not addressed.

The guidelines can be used as necessary to create a development method to minimize the risk of inlet/engine compatibility problems. The degree to which guidelines for descriptor use, assessment techniques, and testing outlined in this document are applied to a specific program should be consistent with the expected severity of the compatibility problem.

 

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Published:
04/27/2017
File Size:
1 file , 740 KB
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This product is unavailable in Ukraine, Russia, Belarus
 

Document History

  1. SAE ARP1420C

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    Gas Turbine Engine Inlet Flow Distortion Guidelines (Stabilized: Apr 2017)

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  2. SAE ARP1420B


    Gas Turbine Engine Inlet Flow Distortion Guidelines

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