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SAE ARP1420

Revision C, April 1, 2017

Complete Document

Gas Turbine Engine Inlet Flow Distortion Guidelines

Includes all amendments and changes through Stabilization Notice (No longer revised / updated) , April 2017


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Product Details:

  • Revision: Revision C, April 1, 2017
  • Published Date: April 2017
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 25
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

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.

AIA/NAS Aerospace Standards