Flow visualization studies of transverse fuel injection patterns in a nonreacting Mach 2 combustorPlanar visualization images are recorded of transverse jet mixing in a supersonic combustor flowfield, without chemical reaction, using laser-induced fluorescence from iodine molecules. Digital image processing and three-dimensional display enable complete representations of fuel penetration boundary and shock surfaces corresponding to several injection geometries and pressures.
Document ID
19870065112
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcdaniel, J. C. (Virginia, University Charlottesville, United States)