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Figure 3
Optical Schlieren images of (a) the shock waves generated by fuel sprays in SF6 gas collected with the injection pressure set at 80 MPa, and (b) the effect of a reflecting wall on the shock front. The spray propagates from left to right along the axis of the injector in the imaging field.

Journal logoJOURNAL OF
SYNCHROTRON
RADIATION
ISSN: 1600-5775
Volume 12| Part 2| February 2005| Pages 197-207
doi:10.1107/S0909049504032297
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