Abstract
The measurements were carried out in a 72 mm square shock tube. A 24° angle wedge was mounted in the shock tube. The shock velocity changed from 600 to 2500 m/sec, the incident pressure being 12 mm Hg. A 1 mm pressure gauge and a thin film platinum gauge were located in the wedge surface. Experimental methods were described in [5]. The experiments were made in air and in carbon dioxyde.
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© 1973 Springer-Verlag Wien
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Bazhenova, T.V. (1973). Measurement. In: Shock Waves in Real Gases. International Centre for Mechanical Sciences, vol 37. Springer, Vienna. https://doi.org/10.1007/978-3-7091-2854-1_6
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DOI: https://doi.org/10.1007/978-3-7091-2854-1_6
Publisher Name: Springer, Vienna
Print ISBN: 978-3-211-81219-8
Online ISBN: 978-3-7091-2854-1
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