Author:
Prasad Phoolan,Krishnan E. V.
Abstract
When we look at photographs of real transonic flows which are predicted to be shockless, we find a very large number of weak shocks almost perpendicular to the streamlines. These are no more than almost-trapped upstream-propagating nonlinear waves. In this paper we try to obtain a simple approximate equation which gives their complete history and takes into account both their turning effect, owing to a non-zero gradient of the fluid velocity in a direction normal to the streamlines, and also the finite radius of curvature of the wave front. We first give a brief discussion of a few results which can be easily obtained from the solution of the approximate equation and then compute the history of two nonlinear pulses by numerically integrating the equation.
Publisher
Cambridge University Press (CUP)
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Reference7 articles.
1. Guderley, K. G. 1962 Theory of Compressible Flow .Pergamon.
2. Prasad, P. 1975 Approximation of the perturbation equations of a quasi-linear hyperbolic system in the neighbourhood of a bicharacteristic.J. Math. Anal. Appl. 50,470.
3. Courant, R. & Hilbert, D. 1962 Methods of Mathematical Physics, vol. 2. Interscience.
4. Spee, B. M. 1971 Investigations on the transonic flow around aerofoils.Nat. Luch-en Ruimtevaartlab. Rep. NLR-TR69122U.
5. Kuo, Y. H. 1951 On the stability of two-dimensional smooth transonic flows.J. Aero. Sci. 18,1.
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