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Theoretical surface velocity distributions on acoustic splitter geometries for an engine inletThe potential-flow velocity distributions on several splitter geometries in an engine inlet and their variation with different splitter leading-edge shapes and distances from the inlet highlight were analyzed. The velocity distributions on the inner and outer surfaces of the splitters are presented for low-speed and cruise conditions. At zero incidence angle, the splitter with the 4-to-1 elliptical leading edge had lower peak velocities and velocity gradients than the splitter with the 2-to-1 elliptical leading edge. The velocity gradients decreased as the distance from the inlet highlight to the splitter leading edge was increased. For a given distance, the peak velocity on the splitter inner surface increased with increasing inlet incidence angle. At an incidence angle of 50 deg, the velocity level and gradients on the inner surface of the splitter in the forward position were sufficiently severe to suggest local separation.
Document ID
19740026341
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Albers, J. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Breunlin, D. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
E-8001
NASA-TM-X-3114
Report Number: E-8001
Report Number: NASA-TM-X-3114
Accession Number
74N34454
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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