Abstract

*Van Dyke, M.D., ''Study of Second-Order Supersonic Flow Theory, NACA TN 2200, 1951. Van Dyke, M.D., Study of Second-Order Supersonic Flow Theory, NACA Kept. 1081, 1952. Martin, J.C. and Gerber, N., The Second-Order Lifting Pressure and Damping in Roll of Sweptback Rolling Airfoils at Supersonic Speeds, Journal of the Aeronautical Sciences, Vol. 20, Oct. 1953, pp. 699-704. Qian, F.X. and Gu, W.K., Accuracy and Application of a Second-Order Theory for Three-dimensional Supersonic and Low Hypersonic Unsteady Flow around a Thin Wing, Acta Aeronautica et Astronautica Sinica, Vol. 2, No. 1, 1981, pp. 1-9. Gu, W.K., The Aerodynamic Behavior of A Harmonically Oscillating Delta Wing in Supersonic and Low Hypersonic Flow Including Nonlinear Thickness Effects, Proceedings of the Third Asian Congress of Fluid Mechanics, Tokyo, Sept. 1-5, 1986. Lebejev, A.A. and Gernobrovkii, L.S., Jinamika Poleta Bespilotnah Letatelineh Apparatov, Oborongiz, SSSR, 1962. Gu, W.K., On Second-Order Theory, Div. 15, Institute of Mechanics, Academia Sinica, Beijing, Res. Rept., Feb. 1981. Murthy, H.S., Subsonic and Transonic Roll Damping Measurements on Basic Finner, Journal of Spacecraft and Rockets, Vol. 19, Jan.-Feb. 1982, pp. 86-87. Shirouzu, M. et al., An Experimental Study on the Induced Rolling Moment due to Wing-Tail Interference and a Rollcontrollable Two-Stage Rocket, NAL TR-793, Dec. 1983.

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