References

Temperature measurement in a compressible flow field using laser-induced iodine fluorescence

10.1364/ol.12.000016 · 1987 · External reference

Laser-induced iodine fluorescence technique for quantitative measurement in a nonreacting, supersonic combustor

10.2514/3.10148 · 1989 · External reference

Planar temperature measurement of compressible flows using laser-induced iodine fluorescence

10.1364/ol.16.000106 · 1991 · External reference

A unified planar measurement technique for compressible flows using laser-induced iodine fluorescence

10.2514/3.11355 · 1993 · External reference

Planar velocity measurement in symmetric flow fields using laser-induced iodine fluorescence

10.1364/ol.19.000216 · 1994 · External reference

Numerical predictions of a rearward-facing-step flow in a supersonic combustor

10.2514/3.23131 · 1989 · External reference

Quantitative characterization of a nonreacting, supersonic combustor using laser-induced iodine fluorescence

10.2514/3.10148 · 1989 · External reference

Staged transverse injection into Mach 2 flow behind a rearward-facing step: a 3-D compressible test case for hypersonic combustor code validation

1991 · External reference

Laser doppler measurements in a Mach 2 flow over a rearward-facing step with staged injection

1991 · External reference

A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer

1988 · External reference

Three dimensional computations of cross-flow injection and combustion in a supersonic flow

1989 · External reference

A validation study of the SPARK Navier-Stokes code for nonreacting scramjet combustor flow fields

1990 · External reference

A high order compact numerical algorithm for supersonic flows

1990 · External reference

Thin layer approximation and algebraic model for separated turbulent flows

1978 · External reference

Unresolved reference

1984 · External reference

Unresolved reference

1988 · External reference

Characteristics of turbulence in a boundary layer with zero pressure gradient

1955 · External reference

Effect of an angular bias on LDA measurements in supersonic turbulent flow

10.1007/bf00196504 · 1988 · External reference

LDA measurements in a Mach 2 flow over a rearward-facing step with staged transverse injection

1992 · External reference

An experimental study of a reattaching supersonic shear layer

1989 · External reference

An experimental study of supersonic flow over rearward-facing step

10.2514/3.3906 · 1967 · External reference

Experimental investigation of supersonic flow separation over a rearward-facing step

1970 · External reference