Abstract
3 Partridge, D. W. and Pecover, B. E., An Application of the RAE Wind-Tunnel/Flight Dynamics Simulator to the Speed Dynamics of a Slender Delta Aircraft (HP 115), Repts. and Memos. 3669, 1969, Aeronautical Research Council, London, England. 4 Engler, P. B. E. and Moss, G. F., Low-Speed Tunnel Tests on a ith Scale Model of the Handley Page HP 115, Repts. and Memos. 3486, 1965, Aeronautical Research Council, London, England. 5 Thompson, J. S. and Fail, R. A., Derivative Measurement on Sting-Mounted Wind-Tunnel Models at RAE Bedford, AGARD Current Paper 17, 1966. 6 Beecham, L. J. and Titchener, I. M., Some Notes on an Approximate Solution for the Free Oscillation Characteristics of Nonlinear Systems Typified by x + F(x,x) = 0, Repts. and Memos. 3651, 1969, Aeronautical Research Council, London, England. 7 KrylofT, N. and Bogoliuboff, N., Introduction to Nonlinear Mechanics, Princeton University Press, Princeton, N.J., 1937. 8 Ross, A. J. and Beecham, L. J., An Approximate Analysis of the Nonlinear Lateral Motion of a Slender Aircraft (HP 115) at Speeds, Repts. and Memos. 3674, 1971, Aeronautical Research Council, London, England. 9 Henderson, J. M., Low Speed Handling of a Slender Delta (HP 115), Journal of the Royal Aeronautical Society, Vol. 69, No. 653, 1965, pp. 311-324. 10 Thompson, J. S., Fail, R. A., and Inglesby, J. V., Low Speed Wind-Tunnel Measurements of the Oscillatory Lateral Stability Derivatives for a Model of the Slender Aircraft (HP 115) Including the Effects of Frequency Parameter, Current Paper 1097, 1969, Aeronautical Research Council, London, England.
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