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SAE ARP1420 Rev C

Current Revision

Gas Turbine Engine Inlet Flow Distortion Guidelines

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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.

SDO SAE: SAE International
Document Number ARP1420
Publication Date April 27, 2017
Language en - English
Page Count 25
Revision Level C
Supercedes
Committee
Publish Date Document Id Type View
April 27, 2017 ARP1420C Revision
March 1, 2002 ARP1420B Revision
Nov. 1, 1998 ARP1420A Revision
March 1, 1978 ARP1420 Revision