Abstract

1 Pitts, W. C., Nielsen, J. N., and Kaattari, G. E., Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic and Supersonic Speeds, Rept. 1307, 1957, NACA. 2 Alien, H. J., Estimation of the Forces and Moments Acting on Inclined Bodies of Revolution, RM A9126, March 1951, NACA. 3 Alien, H. J. and Perkins, E. W., of Flow Over Inclined Bodies of Revolution, RM A50L07, March 1951, NACA. 4 Flax, A. H. and Lawrence, H. P., The Aerodynamics of Low-Aspect-Ratio Wings and Wing-Body Combinations, Rept. CAL-37, Sept. 1951, Cornell Aeronautical Lab., Buffalo, N. Y.; also Proceedings of Third Anglo-American Aeronautical Conference, Brighton, England, Sept. 1951, London, Royal Aeronautical Society, 1952. 5 Eaton, P. T., A Method for Predicting the Static Aerodynamic Characteristics of Low-Aspect-Ratio Configurations, Rept. 2216, June 1966, David Taylor Model Basin, Washington, D. C. 6 Gersten, K., Calculation of Non-Linear Aerodynamic Stability Derivatives of Aeroplanes, Rept. 342, 1961, 1962, Advisory Group for Aeronautical Research and Development, Paris. 7 Franz, G. E., Lift Curve Slopes of Low Aspect Ratio Wings at Transonic Speeds, Applied Mechanics TN AM-TN-2-63, June 1963, North American Aviation, Columbus, Ohio. 8 Douglas Aircraft Co., USAF Stability and Control DATCOM, Rev. W-P AFB, June 1969, Vol. 2, Wright-Patterson Air Force Base, Ohio. 9 Hoerner, S. F., Fluid Dynamic Drag, 2nd ed., Sighard F. Hoerner, Midland Park, N. J., 1958. 10 Dommasch, D. O., Sherby, S. S., and Connolly, T. F., Airplane Aerodynamics, Pitman, New York, 1961. 11 Beil, W. J. et al., Major Developments for the Jet Vane Controlled Bomber Defense Missile, BE-754-S-24, March 1955, Cornell Aeronautical Lab., Buffalo, N. Y.

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