A SHOCK TUBE WITH THE DRIVER GAS PRESSURE INTRODUCED THROUGH AN INLET PORT
Reference44 articles.
1. Mirels, H., (1957) Attenuation in a Shock Tube Due to the Unsteady-Boundary-Layer Action, NACATR-1333, pp. 1-19. 2. Goulard, R., (1958) On Catalytic Recombination Rates in Hypersonic Stagnation Heat Transfer, Jet Propulsion, pp. 737-745. 3. Briassulis, G., Agui, J.H., Andreopoulos, J., and Watkins, C.B., (1996) A Shock Tube Research Facility for High-Resolution Measurements of Compressible Turbulence, Experimental Thermal and Fluid Science, 13(4), pp. 430-446 4. Daru, V., and Tenaud, C., (2001) Evaluation of TVD High Resolution Schemes for Unsteady Viscous Shocked Flows, Computers Fluids, 30, pp. 89-113. 5. Gamezo, V.N., Khokhlov, A.M., and Oran, E.S., (2001) The Influence of Shock Bifurcations on Shock-Flame Interactions and DDT, Combustion and Flame, 126, pp. 1810-1826.
|
|