Some methods of leak testing in high-vacuum systems and components : W. Steckelmacher, R. & D.24, 14 (Aug. 1963)

Abstract

Unsteady three-dimensional numerical simulation on a single spinning detonation in a circular tube are presented in order to understand the effects of energy release of the mixture on the detonation structure. Overall structures of the spinning detonations such as the shock structure around the spin head, the long pressure trail, and the track angle on the wall are not affected by these effects because they depend on the specific heat ratio of the products which has approximately a constant value. The calculated averaged detonation velocities on the symmetry axis during one cycle decrease inversely with an exponential curve to become the value lower than the CJ detonation velocity. Those for p0 = 0.1 MPa and p0 = 0.01 MPa become approximately 0.98 DCJ and 0.92 DCJ, respectively, because the energy release in the CJ state for p0 = 0.01 MPa is 10% lower than that for p0 = 0.1 MPa. The state of gas behind the head of spinning detonation is also evaluated by the classical oblique shock theory and equilibrium calculation by using the track angle, shock wave angle, and detonation velocity in order to compare with the present and other researcher’s numerical results. The effects of the energy release in the mixture are large on the strength of the transverse detonation.