Publication Date:
2019-06-27
Description:
The application, installation, and monitoring of dynamic strain gage instrumentation on the rotating fan blades for subsonic stalled flutter mode of the first fan rotor are described. The engine installation, the modifications to the engine controls to obtain off schedule operation of the fan, engine aerodynamic instrumentation, and general data acquisition systems are discussed.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-TM-X-3508
,
E-9088
Format:
application/pdf
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