Simultaneous Raman-Rayleigh-LIF Measurements and Numerical Modeling Results of a Lifted H2/N2 Turbulent Jet Flame in a Vitiated CoflowAn experimental and numerical investigation is presented of a H2/N2 turbulent jet flame burner that has a novel vitiated coflow. The vitiated coflow emulates the recirculation region of most combustors, such as gas turbines or furnaces. Additionally, since the vitiated gases are coflowing, the burner allows for exploration of recirculation chemistry without the corresponding fluid mechanics of recirculation. Thus the vitiated coflow burner design facilitates the development of chemical kinetic combustion models without the added complexity of recirculation fluid mechanics. Scalar measurements are reported for a turbulent jet flame of H2/N2 in a coflow of combustion products from a lean ((empty set) = 0.25) H2/Air flame. The combination of laser-induced fluorescence, Rayleigh scattering, and Raman scattering is used to obtain simultaneous measurements of the temperature, major species, as well as OH and NO. Laminar flame calculation with equal diffusivity do agree when the premixing and preheating that occurs prior to flame stabilization is accounted for in the boundary conditions. Also presented is an exploratory pdf model that predicts the flame's axial profiles fairly well, but does not accurately predict the lift-off height.
Document ID
20030014613
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Cabra, R. (California Univ. Berkeley, CA United States)
Chen, J. Y. (California Univ. Berkeley, CA United States)
Dibble, R. W. (California Univ. Berkeley, CA United States)
Hamano, Y. (Ishikawajima-Harima Heavy Industries Co. Ltd. Tokyo, Japan)
Karpetis, A. N. (Sandia National Labs. Livermore, CA United States)
Barlow, R. S. (Sandia National Labs. Livermore, CA United States)
Date Acquired
September 7, 2013
Publication Date
December 1, 2002
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:212081E-13734WSS/CI-2001-288NASA/CR-2002-212081Report Number: NAS 1.26:212081Report Number: E-13734Report Number: WSS/CI-2001-288Report Number: NASA/CR-2002-212081