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Formation of gasdynamic flow for plates colliding at a sharp angle

Journal Article · · Combust., Explos. Shock Waves (Engl. Transl.); (United States)
DOI:https://doi.org/10.1007/BF00750713· OSTI ID:6817647
The authors experimentally study the dynamics of the accumulation of a bunch of shock compressed gas, formed when a plate is propelled at a substrate by a sliding detonation wave, propagating with a velocity of U/sub 0/ greater than 6 km/sec. The detonation velocity was chosen to exceed the velocity of sound in the plate and substrate materials, which ensured that particles and cumulative jets from the region of the point of contact would not be generated. A diagram of the experiments is shown. The study shows the existence of three states of gasdynamic flow (with stable accumulation of plasma, the stall state, and with no accumulation); the velocity of the direct shock wave formed exceeds the adiabatic velocity and increases as the gap size decreases; and, the strong solution is realized behind the front of the oblique shock wave -- the parameters of the bunch of shock-compressed gas formed are independent of the angle of flight of the propelled plate.
OSTI ID:
6817647
Journal Information:
Combust., Explos. Shock Waves (Engl. Transl.); (United States), Journal Name: Combust., Explos. Shock Waves (Engl. Transl.); (United States) Vol. 22:1; ISSN CESWA
Country of Publication:
United States
Language:
English