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Simultaneous Temperature and Velocity Measurements in a Large-Scale, Supersonic, Heated JetTwo laser-based measurement techniques have been used to characterize an axisymmetric, combustion-heated supersonic jet issuing into static room air. The dual-pump coherent anti-Stokes Raman spectroscopy (CARS) measurement technique measured temperature and concentration while the interferometric Rayleigh scattering (IRS) method simultaneously measured two components of velocity. This paper reports a preliminary analysis of CARS-IRS temperature and velocity measurements from selected measurement locations. The temperature measurements show that the temperature along the jet axis remains constant while dropping off radially. The velocity measurements show that the nozzle exit velocity fluctuations are about 3% of the maximum velocity in the flow.
Document ID
20080020526
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Danehy, P. M.
(NASA Langley Research Center Hampton, VA, United States)
Magnotti, G.
(George Washington Univ. Newport News, VA, United States)
Bivolaru, D.
(George Washington Univ. Newport News, VA, United States)
Tedder, S.
(NASA Langley Research Center Hampton, VA, United States)
Cutler, A. D.
(George Washington Univ. Newport News, VA, United States)
Date Acquired
August 24, 2013
Publication Date
May 12, 2008
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 55th JANNAF Propulsion Meeting/42nd Combustion/30th Airbreathing Propulsion/30th Exhaust Plume Technology/ 24th Propulsion Systems Hazards/12th SPIRITS User Group Joint Subcommittee Meeting
Location: Newton, MA
Country: United States
Start Date: May 12, 2006
End Date: May 16, 2006
Sponsors: Department of the Navy, Department of the Army, NASA Headquarters, Department of the Air Force
Funding Number(s)
WBS: WBS 599489.02.07.07.06.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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