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Flow-field Survey of an Empennage Wake Interacting with a Pusher PropellerThe flow field between a model empennage and a 591-mm-diameter pusher propeller was studied in the Ames 7- by 10-Foot Wind Tunnel with directional pressure probes and hot-wire anemometers. The region probed was bounded by the empennage trailing edge and downstream propeller. The wake properties, including effects of propeller operation on the empennage wake, were investigated for two empennage geometries: one, a vertical tail fin, the other, a Y-tail with a 34 deg dihedral. Results showed that the effect of the propeller on the empennage wake upstream of the propeller was not strong. The flow upstream of the propeller was accelerated in the streamwise direction by the propeller, but the empennage wake width and velocity defect were relatively unaffected by the presence of the propeller. The peak turbulence in the wake near the propeller tip station, 0.66 diameter behind the vertical tail fin, was approximately 3 percent of the free-stream velocity. The velocity field data can be used in predictions of the acoustic field due to propeller-wake interaction.
Document ID
19890002323
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Horne, W. Clifton
(NASA Ames Research Center Moffett Field, CA, United States)
Soderman, Paul T.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1988
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.15:101003
NASA-TM-101003
A-88185
Report Number: NAS 1.15:101003
Report Number: NASA-TM-101003
Report Number: A-88185
Accession Number
89N11694
Funding Number(s)
PROJECT: RTOP 505-61-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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