Abstract
5 Jones, R. T., Theoretical Determination of the Minimum Drag of Airfoils at Supersonic Speeds, Journal of the Aeronautical Sciences, Vol. 19, No. 12, Dec. 1952, pp. 813-822. 6 Carmichael, R. L., Castellano, C. R., and Chen, C. F., Use of Finite Element Methods for Predicting the Aerodynamics of WingBody Combinations, Analytic Methods in NASA SP 228, 1969, pp. 37-51. 7 Smith, J. H. B., Lift/Drag Ratios of Optimized Elliptic Wings at Supersonic Speeds, The Aeronautical Quarterly, Vol. XII, Aug. 1961, pp. 201-218. 8 Jones, R. T., Aerodynamic Design for Supersonic Speeds, Proceedings of the First International Congress in the Aeronautical Sciences, Advances in Aeronautical Sciences, Pergamon Press, New York, 1959, pp. 34-51. 9 Kuchemann, D., Aircraft Shapes and Their Aerodynamics, Proceedings of the 2nd I.C.A.S., Advances in Aeronautical Sciences, Vol. 34, Pergamon Press, New York, 1962, pp. 221-252. 10 Holdaway, G. H. and Hatfield, E. W., Transonic of Yawed Wings of Aspect Ratios 3 and 6 With a Sears-Haack Body and With Symmetrical and Asymmetrical Bodies Indented for a Mach Number of 1.2, RM A58C03, 1958, NACA. 11 Campbell, J. P. and Drake, H. M., Investigation of Stability and Control Characteristics of an Airplane Model With Skewed Wing in the Langley Free-Flight Tunnel, TN 1208, 1947, NACA. 12 Lee, G. H., comments appended to Kuchemann, D., Aircraft Shapes and Their Aerodynamics, Proceedings of the 2nd I.C.A.S. Advances in Aeronautical Sciences, Vol. 3-4, Pergamon Press, New York, 1962, pp. 221-252. 13 Lee, G. H., Slewed Wing Supersonics, The Aeroplane, Vol. 100, March 1961, pp. 240-241.
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