Effect of yaw on the starting point of curvature for reflected diffracted shock wave (subsonic and sonic cases) |
| |
Authors: | R S Srivastava |
| |
Institution: | (1) Defence Science Centre, New Delhi, India;(2) Present address: A-3/260, Janakpuri, New Delhi, 110058, India |
| |
Abstract: | Lighthill (Proc. R. Soc. A 198, 454–470, 1949) considered the diffraction of a normal shock wave passing over a small bend. The bend being small Lighthill
was able to linearize the flow equations and solved the problem through several mathematical techniques. Following Lighthill
(Proc. R. Soc. A 198, 454–470, 1949), Srivastava and Chopra (J. Fluid Mech. 40, 821–831, 1970) extended the work to the diffraction of oblique shock waves. Srivastava (AIAAJ 33, 2230–2231, 1995) considered the problem of starting point of curvature and extended the work to yawed wedges (Srivastava
in Proceedings of the 14th International Mach reflection symposium Sun Marina Hotel, Yonezawa, Japan, 1–5 October 2000, pp.
225–249, 2002). Srivastava (Shock waves 13, 323–326, 2003) considered the problem for starting point of curvature when the relative outflow behind reflected shock before
diffraction has been subsonic and sonic. The present work is an extension of the work published in Srivastava (Shock waves
13, 323–326, 2003) when the wedge has been yawed through an angle. The results have been obtained for two angles χ = 60° and
χ = 40° (χ is the angle of yaw).
|
| |
Keywords: | Diffraction Reflection Yaw Curvature |
本文献已被 SpringerLink 等数据库收录! |
|