Abstract
Fig. 1 Typical curved waverider (——) and a caret wing (-) and the supporting shock waves: 7 = 1.4; A/o>= 10; a = 25 deg.; fto = 0.1; 62=-2 References ^essiter, A. F., Lift of Slender Delta Wings According to Newtonian Theory, AIAA Journal, Vol. 1, No. 4, 1963, pp. 794-802. Hemdan, H. T., and Hui, W. H., Unsteady and Steady Aerodynamic Forces of Slender Delta Wings According to Newtonian Theory, Canadian Aeronautics and Space Journal, Vol. 23, No. 4, 1976, pp. 238-251. Malmuth, N. D., Three-Dimensional Perturbations on Hypersonic Wedge Flow, AIAA Journal, Vol. 2, No. 8, 1964, pp. 1383-1389. Hui, W. H., Supersonic and Hypersonic Flow with Attached Shock Waves over Delta Wings, Proceedings of the Royal Society of London, Series A, Vol. 325, 1971, pp. 251-267. Hemdan, H. T., Waverider Configurations According to Thin Shock-layer Theory, Acta Astronautica, Vol. 21, No. 8, 1990, pp. 571-582.
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