Dual-Pump CARS Measurements in the University of Virginia's Dual-Mode Scramjet: Configuration "C"Measurements have been conducted at the University of Virginia Supersonic Combustion Facility in configuration C of the dual-mode scramjet. This is a continuation of previously published works on configuration A. The scramjet is hydrogen fueled and operated at two equivalence ratios, one representative of the scram mode and the other of the ram mode. Dual-pump CARS was used to acquire the mole fractions of the major species as well as the rotational and vibrational temperatures of N2. Developments in methods and uncertainties in fitting CARS spectra for vibrational temperature are discussed. Mean quantities and the standard deviation of the turbulent fluctuations at multiple planes in the flow path are presented. In the scram case the combustion of fuel is completed before the end of the measurement domain, while for the ram case the measurement domain extends into the region where the flow is accelerating and combustion is almost completed. Higher vibrational than rotational temperature is observed in those parts of the hot combustion plume where there is substantial H2 (and hence chemical reaction) present.
Document ID
20130003230
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Cutler, Andrew D. (George Washington Univ. Newport News, VA, United States)
Magnotti, Gaetano (George Washington Univ. Newport News, VA, United States)
Cantu, Luca (George Washington Univ. Newport News, VA, United States)
Gallo, Emanuela (George Washington Univ. Newport News, VA, United States)
Danehy, Paul M. (NASA Langley Research Center Hampton, VA, United States)
Rockwell, Robert (Virginia Univ. Charlottesville, VA, United States)
Goyne, Christopher (Virginia Univ. Charlottesville, VA, United States)
McDaniel, James (Virginia Univ. Charlottesville, VA, United States)
Date Acquired
August 27, 2013
Publication Date
January 7, 2013
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2013-0335NF1676L14873Report Number: AIAA Paper 2013-0335Report Number: NF1676L14873
Meeting Information
Meeting: 51st AIAA Aerospace Sciences Meeting
Location: Grapevine, TX
Country: United States
Start Date: January 7, 2013
End Date: January 10, 2013
Funding Number(s)
WBS: WBS 599489.02.07.07.04.11.01 CONTRACT_GRANT: FA 9550-09-1-0611