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Supersonic Coaxial Jet Experiment for CFD Code ValidationA supersonic coaxial jet facility has been designed to provide experimental data suitable for the validation of CFD codes used to analyze high-speed propulsion flows. The center jet is of a light gas and the coflow jet is of air, and the mixing layer between them is compressible. Various methods have been employed in characterizing the jet flow field, including schlieren visualization, pitot, total temperature and gas sampling probe surveying, and RELIEF velocimetry. A Navier-Stokes code has been used to calculate the nozzle flow field and the results compared to the experiment.
Document ID
20040086859
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Cutler, A. D. (George Washington Univ. Hampton, VA, United States)
Carty, A. A. (George Washington Univ. Hampton, VA, United States)
Doerner, S. E. (George Washington Univ. Hampton, VA, United States)
Diskin, G. S. (NASA Langley Research Center Hampton, VA, United States)
Drummond, J. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 99-3588
Report Number: AIAA Paper 99-3588
Meeting Information
Meeting: 30th AIAA Fluid Dynamics Conference
Location: Norfolk, VA
Country: United States
Start Date: June 28, 1999
End Date: July 1, 1999
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NCC1-217
Distribution Limits
Public
Copyright
Public Use Permitted.

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