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SAE ARP 1420C:2017-04-27
Gas Turbine Engine Inlet Flow Distortion Guidelines (Stabilized: Apr 2017)More info
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.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| ICS | 49.050 : Aerospace engines and propulsion systems |
| Number of pages | 25 |
| Replace | SAE ARP 1420B:2011-07-20 |
| Set | AEROPAKS10U-10 |
| Year | 2017 |
| Document history | SAE ARP 1420B:2011-07-20 |
| Country | USA |
| Keyword | SAE 1420;SAE ARP1420C;SAE ARP1420C;SAE ARP 1420 |