Abstract
Lighthill (1949) investigated the diffraction of a normal shock wave past a small bend. Chester(1954) extended the work of Lighthill to include infinte wedges at yaw. The work presented in this chapter is that of Smyrl(1963) and is concerned with a plane shock wave meeting a thin two dimensional aerofoil moving in the opposite direction at supersonic speed. The effect of yaw has also been included in the analysis.
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References
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Chester, W.The diffraction and reflection of shock wave. Quar. Jourl. Mech Appl. Maths, 7, 57–82. (1954)
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© 1994 Springer Science+Business Media Dordrecht
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Srivastava, R.S. (1994). Shock Interaction with Moving Aerofoil. In: Interaction of Shock Waves. Fluid Mechanics and Its Applications, vol 22. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-1086-0_7
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DOI: https://doi.org/10.1007/978-94-011-1086-0_7
Publisher Name: Springer, Dordrecht
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