A new experimental approach to the study of the two-dimensional compressibl
e flow phenomena is presented. In this technique, a variety of compressible
flows were generated by bursting plane vertical soap films. An aureole and
a "shock wave" preceding the rim of the expanding hole were clearly observ
ed using traditional highspeed flash photography and a fast line-scan charg
e coupled device (CCD) camera. The moving shock wave images obtained from t
he line-scan CCD camera were similar to the x-t diagrams in gas dynamics. T
he moving shock waves cause thickness jumps and induce supersonic flows. Ph
otographs of the supersonic flows over a cylinder and a wedge are presented
. The results suggest clearly the feasibility of the "soap film shock tube"
.