Title :
N2/O2/H2 dual-pump cars: validation experiments
Author :
O´Byrne, Sean ; Daneh, P.M. ; Cutler, A.D.
Author_Institution :
NASA Langley Res. Center, Hampton, VA, USA
Abstract :
The dual-pump coherent anti-Stokes Raman spectroscopy (CARS) method is used to measure temperature and the relative species densities of N2, O2 and H2 in two experiments. Average values and root-mean-square (RMS) deviations are determined. Mean temperature measurements in a furnace containing air between 300 and 1800 K agreed with thermocouple measurements within 26 K on average, while mean mole fractions agree to within 1.6% of the expected value. The temperature measurement standard deviation averaged 64 K while the standard deviation of the species mole fractions averaged 7.8% for O2 and 3.8% for N2, based on 200 single-shot measurements. Measurements have been performed in a hydrogen-air flat-flame burner for fuel-lean and fuel-rich conditions. A preliminary comparison is shown between the fitted data and an adiabatic, equilibrium computation. For fuel-lean conditions, good agreement was found for temperature. Temperatures measured under fuel-rich conditions were about 50 K higher than the computation. Mole-fractions for N2 agreed with the computation to within 3%. Measured O2 mole fractions were systematically high while measured H2 mole fractions were systematically low by 10-15% compared to the computation. For an equivalence ratio of 2.8, the standard deviation of 58 single-shot temperature measurements was 108 K, or 5.8%, and the standard deviations of H2 and N2 mole fractions were 9.8% and 3.8% of the measured values, respectively.
Keywords :
coherent antiStokes Raman scattering; computational fluid dynamics; density measurement; flames; flow measurement; heat transfer; hydrogen; nitrogen; optical pumping; oxygen; temperature measurement; thermocouples; 108 K; 26 K; 300 to 1800 K; 64 K; H2; N2; O2; RMS deviations; adiabatic equilibrium computation; coherent antiStokes Raman spectroscopy; dual pump CARS; furnaces; hydrogen air flat flame burner; mean mole fraction; root mean square deviations; standard deviation; temperature measurement; thermocouple measurements; Computational fluid dynamics; Engines; Fluid flow measurement; Frequency; Laser excitation; Measurement standards; NASA; Raman scattering; Spectroscopy; Temperature measurement;
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on
Print_ISBN :
0-7803-8149-1
DOI :
10.1109/ICIASF.2003.1274879