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D.R. Eklund, D.G. Fletcher, R.J. Hartfield, G.B. Northam, C.L. Dancey
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Temperature measurement in a compressible flow field using laser-induced iodine fluorescence
10.1364/ol.12.000016 · 1987
Laser-induced iodine fluorescence technique for quantitative measurement in a nonreacting, supersonic combustor
10.2514/3.10148 · 1989
Planar temperature measurement of compressible flows using laser-induced iodine fluorescence
10.1364/ol.16.000106 · 1991
A unified planar measurement technique for compressible flows using laser-induced iodine fluorescence
10.2514/3.11355 · 1993
Planar velocity measurement in symmetric flow fields using laser-induced iodine fluorescence
10.1364/ol.19.000216 · 1994
Numerical predictions of a rearward-facing-step flow in a supersonic combustor
10.2514/3.23131 · 1989
Quantitative characterization of a nonreacting, supersonic combustor using laser-induced iodine fluorescence
10.2514/3.10148 · 1989
Staged transverse injection into Mach 2 flow behind a rearward-facing step: a 3-D compressible test case for hypersonic combustor code validation
1991
Laser doppler measurements in a Mach 2 flow over a rearward-facing step with staged injection
1991
A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer
1988
Three dimensional computations of cross-flow injection and combustion in a supersonic flow
1989
A validation study of the SPARK Navier-Stokes code for nonreacting scramjet combustor flow fields
1990
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10.1007/bf00196504 · 1988
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