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• W2079438105 abstract "Communications on Pure and Applied MathematicsVolume 7, Issue 1 p. 1-10 Article Mathematical methods in compressible flow theory M. J. Lighthill, M. J. Lighthill University of Manchester, EnglandSearch for more papers by this author M. J. Lighthill, M. J. Lighthill University of Manchester, EnglandSearch for more papers by this author First published: February 1954 https://doi.org/10.1002/cpa.3160070102Citations: 4AboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onEmailFacebookTwitterLinkedInRedditWechat Bibliography 1 Gadd, G. E., On the interaction with a completely laminar boundary layer of a shock wave generated in the mainstream, Aeronautical Research Council, Report No. 15, 100 (unpublished). 2 Whitham, G. B., The flow pattern of a supersonic projectile, Communications on Pure and Applied Mathematics, Volume 5, 1952, p. 301. 3 Oswstitsch, K., and Wieghardt, K., Theoretical analysis of stationary potential flows and boundary layers at high speed, National Advisory Committee for Aeronautics, Technical Memorandum No. 1189, 1948, reprinted from German wartime report, 1941. 4 Liepmann, H. W., Roshko, A., and Dhawan, S., On the reflection of shock waves from boundary layers, Guggenheim Aeronautical Laboratory, California Institute of Technology, Report, 1949, National Advisory Committee for Aeronautics, Technical Note No. 2334, 1951. 5 Lees, L., Interaction between the laminar boundary layer over a plane surface and an incident oblique shock wave, Princeton University Aeronautical Engineering Laboratory, Report No. 143, 1949. 6 Lees, L., and Crocco, L., A mixing theory for the interaction between dissipative flows and nearly-isentropic streams, Princeton University Aeronautical Engineering Laboratory, Report No. 187, 1952. 7 Howarth, L., The propagation of steady disturbances in a supersonic stream bounded on one side by a parallel subsonic stream, Proceedings of the Cambridge Philosophical Society, Volume 44, 1948, p. 380. 8 Tsien, H. S., and Finston, M., Interaction between parallel streams of subsonic and supersonic velocities, Journal of the Aeronautical Sciences, Volume 16, 1949, p. 515. 9 Lighthill, M. J., Reflection at a laminar boundary layer of a weak steady disturbance to a supersonic stream, neglecting viscosity and heat conduction, Quarterly Journal of Mechanics and Applied Mathematics, Volume 3, 1950, p. 303. 10 Lighthill, M. J., On boundary layers and upstream influence, Parts I and II, Proceedings of the Royal Society, Volume 217, pp. 344–357 and 378–407. 11 Lighthill, M. J., The energy distribution behind decaying shocks. I, Plane waves, Philosophical Magazine, Volume 41, 1950, p. 1101. 12 Whitham, G. B., The behaviour of supersonic flow past a body of revolution, far from the axis, Proceedings of the Royal Society, Volume 201, 1950, p. 89. 13 Lighthill, M. J., A technique for rendering approximate solutions to physical problems uniformly valid, Philosophical Magazine, Volume 40, 1949, p. 1179. 14 Warren, C. H. E., Sonic bangs, a quantitative explanation, Royal Aircraft Establishment, Technical Note No. 2192, Farnborough, 1952. 15 Allen, H. J., and Perkins, E. W., A study of effects of viscosity on flow over slender inclined bodies of revolution, National Advisory Committee for Aeronautics, Report No. 1048, 1951. 16 Lees, L., The stability of the laminar boundary layer in a compressible fluid, National Advisory Committee for Aeronautics, Technical Note No. 1360, July 1947. 17 Lighthill, M. J., On sound generated aerodynamically. I, General theory, Proceedings of the Royal Society, Volume 211, 1952, p. 564. 18 Westley, R., and Lilley, G. M., An investigation into the noise field from a small jet and methods for its reduction, College of Aeronautics, Report No. 53, Cranfield, 1952. 19 Gerrard, J. H., Experiments on jet noise, to appear. 20 Lassiter, L. W., and Hubbard, H. H., Experimental studies of noise from subsonic jets in still air, National Advisory Committee for Aeronautics, Technical Note No. 2757, 1952. 21 Fitzpatrick, H. M., and Lee, R., Measurements of noise radiated by subsonic air jets, David Taylor Model Basin, Report No. 835, 1952. 22 Proudman, I., The generation of noise by isotropic turbulence, Proceedings of the Royal Society, Volume 214, 1952, p. 119. 23 Lighthill, M. J., On sound generated aerodynamically. II. Turbulence as a source of sound, to appear in Proceedings of the Royal Society. Citing Literature Volume7, Issue1February 1954Pages 1-10 ReferencesRelatedInformation" @default.
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