| || A Note on the Interaction of a Shock Wave with a Curved Boundary
Author : Biswas, R.K.
Source : Defence Science Journal ; Vol:20(1) ; 1970 ; pp 59-62
Subject : 623.454.833 Shock Waves
Keywords : Shock wave ;Pressure field;Arbitrary plane
Abstract : The analytical expression for the pressure field behind an arbitrary plane shock-wave which encounters a curved boundary at nearly incidence had been obtained. The pressure distribution on the surface for different shocks is calculated and compared with that of a wedge.
| || On the Interaction of Oblique Shock Wave with a Yawed Wedge
Author : Biswas, R.K.;Srivastava, R.S.
Source : Defence Science Journal ; Vol:16(4) ; 1966 ; pp 231-234
Subject : 620.261 Explosives ;623.454.833 Shock Waves
Keywords : Reflected shock;Yaw ;Shock Waves
Abstract : When an oblique shock configuration encounters an infinite yawed wedge, it has been found that the region between the incident and the reflected shock, called intermediate region, remains undisturbed for any angle of yaw.