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Nonlinear wave propagation on an arbitrary steady transonic flow

Published online by Cambridge University Press:  29 March 2006

Phoolan Prasad
Affiliation:
School of Mathematics, University of Leeds Present address: Department of Applied Mathematics, Indian Institute of Science, Bangalore 560012, India.

Abstract

Here, we have studied the propagation of an arbitrary disturbance bounded in space on an arbitrary two- or three-dimensional transonic flow. First we have presented a general theory valid for an arbitrary system of n first-order quasi- linear partial differential equations and then used the theory for the special case of gasdynamic equations. If a disturbance is created in the neighbourhood of a sonic point, only a part of the disturbance stays in the transonic region and it is bounded by a wave front perpendicular to the streamlines. This part of the disturbance is governed by a very simple partial differential equation and the problem essentially reduces to the discussion of one-dimensional waves. The disturbance decays in the neighbourhood of the points where the flow acceler- ates from a subsonic state to a supersonic state and it attains a steady state where the flow is decelerating.

Type
Research Article
Copyright
© 1973 Cambridge University Press

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References

Bhatnagar, P. L. & Prasad, P. 1971 Proc. Roy. Soc. A322, 45.
Courant, R. & Hilbert, D. 1962 Methods of Mathematical Physics, vol. 2. Interscience.
Kantrowitz, A. R. 1947 The formation and stability of normal shock waves in channel flow. N.A.C.A. Tech. Note no. 1225.Google Scholar
Kantrowitz, A. R. 1958 One-dimensional treatment of non-steady gas dynamics. Fundamentals of Gasdynamics (ed. W. D. Emmons), part C. Oxford University Press.
Kulikovskii, A. G. & Slobodeina, F. A. 1967 Prikl. Math. Mech. 31, 623.
Kuo, Y.H. 1951 J. Aero. Sci. 18, 1.
Landau, L. D. & Lifshitz, E. M. 1959 Fluid Mechanics. Pergamon.
Morawetz, C. S. 1964 Cornmun. Pure. Appl. Math. 17, 357.
Nieulwand, G. Y. 1966 Theoretical design of shock free transonic flow mound aerofoil sections. Aerospace Proc. 1966, 5B Congress Int. Counc. Aero. Sci.Google Scholar
Nieulwand, G.Y. & Spee, B. M. 1968 Transonic shock free flow, fact or fiction? Agard Specialists' Meeting on Transonic Plows (Paris), NLR MP 68004.Google Scholar
Pearcey, H. H. 1962 Adv. Aeron. Sci. 3, 277.
Spee, B. M. 1971 Nationaal Lucht-en Ruimtmaartlabotorium, NLRTR 69122 U.