NDLI: Effect of yaw on the starting point of curvature for reflected diffracted shock wave (subsonic and sonic cases)

Content Provider	Springer Nature Link
Author	Srivastava, R. S.
Copyright Year	2007
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).
Ending Page	212
Page Count	4
Starting Page	209
File Format	PDF
ISSN	09381287
e-ISSN	14322153
Journal	Shock Waves
Issue Number	3
Volume Number	17
Language	English
Publisher	Springer-Verlag
Publisher Date	2007-08-15
Publisher Place	Berlin, Heidelberg
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Thermodynamics Mechanics, Fluids, Thermodynamics Fluids Diffraction Solid State Physics and Spectroscopy Condensed Matter Reflection Acoustics Curvature Yaw
Content Type	Text
Resource Type	Article
Subject	Physics and Astronomy Mechanical Engineering

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