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SAE AIR 1935:2007-11-07

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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 Rigs

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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