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Pratt & Whitney Two Dimensional HSR Nozzle Test in the NASA Lewis 9- By 15- Foot Low Speed Wind Tunnel: Aerodynamic ResultsThis paper discusses a test that was conducted jointly by Pratt & Whitney Aircraft Engines and NASA Lewis Research Center. The test was conducted in NASA's 9- by 15-Foot Low Speed Wind Tunnel (9x15 LSWT). The test setup, methods, and aerodynamic results of this test are discussed. Acoustical results are discussed in a separate paper by J. Bridges and J. Marino.
Document ID
19990110611
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wolter, John D. (NASA Lewis Research Center Cleveland, OH United States)
Jones, Christopher W. (Pratt and Whitney Aircraft East Hartford, CT United States)
Date Acquired
August 19, 2013
Publication Date
September 1, 1999
Publication Information
Publication: First NASA/Industry High Speed Research Program Nozzle Symposium
Subject Category
Aircraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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