An explosive shock tube
Journal Article
·
· High Temp. (USSR) (Engl. Transl.), v. 10, no. 6, pp. 1149-1152
OSTI ID:4365023
Experiments with a model explosive shock tube are described. Flow of a dense air plasma with speed 25-l0 km/sec is obtained by means of an explosive gas compressor. Photographs of flow over models were taken when the flow behind the shock wave becomes opaque. The experiments were conducted in a laboratory explosion chamber, (auth)
- Research Organization:
- Institute of Nuclear Physics, Siberian Branch, Academy of Sciences of the USSR
- NSA Number:
- NSA-29-014467
- OSTI ID:
- 4365023
- Journal Information:
- High Temp. (USSR) (Engl. Transl.), v. 10, no. 6, pp. 1149-1152, Journal Name: High Temp. (USSR) (Engl. Transl.), v. 10, no. 6, pp. 1149-1152; ISSN HITEA
- Country of Publication:
- United States
- Language:
- English
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