Velocity measurement in a dual-mode supersonic combustor using particle image velocimetry
Author:
Affiliation:
1. Virginia, Univ., Charlottesville
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1761
Reference36 articles.
1. McClinton, C.R.,Holland, S.D.,Rock, K.E, Engelund, W.C.,Voland, R.T., Huebner, L.D.,and Rogers, R.C. "Hyper-X Wind Tunnel Program," AIAA Paper 98-0553,Jan.1998.
2. 2Goyne, C.P.,McDaniel, J.C.,Quagliaroli, T.M., Krauss, R.H., and Day, S.W. "Dual-Mode Combustion of Hydrogen in a Mach 5, Continuous-Flow Facility," accepted for publication in Journal of Propulsion and Power,2001.
3. Experimental and numerical investigation on steam-vitiated supersonic hydrogen combustion
4. OH Planar Laser-Induced Fluorescence Velocity Measurements in a Supersonic Combustor
5. 5Rodriguez, C.G.,White, J.A.,and Riggins, D.W. "Three-Dimensional Effects in Modeling of Dual-Mode Scramjets," AIAAPaper 2000-3704,July,2000.
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