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SAE AIR 1935:2007-11-07
Methods of Controlling Distortion of Inlet Airflow During Static Acoustical Tests of Turbofan Engines and Fan RigsMore info
This Aerospace Information Report provides guidelines for hardware design. Guidelines on such items as engine types, test arrangements, and test purposes that would benefit from the use of an inflow control device during static noise testing are outside the scope of this report.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2007-11-07 |
| ICS | 17.140.30 : Noise emitted by means of transport 49.050 : Aerospace engines and propulsion systems |
| Number of pages | 15 |
| Set | AEROPAKS10U-10 |
| Year | 2007 |
| Document history | |
| Country | USA |
| Keyword | SAE 1935;SAE AIR1935;SAE AIR1935;SAE AIR 1935 |