Single-shot color schlieren photography of supersonic flow phenomena r
equires a technically complex flash light source. In particular, it sh
ould be of ultrashort duration to minimize motion blur, of high intens
ity to expose regular color film with only one flash, and should emit
an almost ''white'' spectrum to provide the full scale of possible hue
s. Furthermore, matching Settles' (1970) direction indicating color di
ssection method the source should be of an areal geometry to uniformly
illuminate a tricolor filter in the source plane. Two different types
of light sources have been constructed and compared to each other: an
array of five Xe-filled linear flash lamps and a module of eight clos
ely stacked U-shaped loops of micro gliding sparks. The spark module c
onsists of a total of 280 individual micro gliding discharges which ar
e all arranged uniformly within an area of 40 x 40 mm. Connected in a
series and pulsed by a modified eight-stage 15 kV Marx-surge generator
they are operated in a nitrogen gas atmosphere doped with xenon by ab
out 15% of volume at a total pressure of 1.5 bar. The emitted flash ha
s a peak light intensity of 29 Mcd and a flash duration of 292 ns FWHM
. Advantageously in comparison to flash lamps, the flash of a gliding
spark module is shorter and free of oscillatory afterglow, thus provid
ing dear and sharp schlieren photos of shock waves which, for example,
are purged from preceding ''phantom shock fronts''.