Browse Standards ARP1420B
Historical REAFFIRMED 2011-07-20

Gas Turbine Engine Inlet Flow Distortion Guidelines ARP1420B

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.
ARP1420C
2017-04-27
Latest
Stabilized
ARP1420B
2011-07-20
Historical
Reaffirmed
ARP1420A
1998-11-01
Historical
Revised
ARP1420
1978-03-01
Historical
Issued

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