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- W1990888046 abstract "References 1Rodden, W. P., and Love, J. R., “Equations of Motion of an Elastic Flight Vehicle Utilizing Static Aeroelastic Characteristics of the Restrained Vehicle,” AIAA Paper 84-0986,May 1984. 2Wykes, J. H., and Lawrence, R. E., “Aerothermoelasticity: Its Impact on Stability and Control of Winged Aerospace Vehicles,” Journal of Aircraft, Vol. 2, No. 6, 1965, pp. 517–526. 3Sheena, Z., and Karpel, M., “Static Aeroelastic Analysis Using Aircraft VibrationModes,”Proceedings of the 2nd InternationalSymposiumon Aeroelasticity and Structural Dynamics, 1985, pp. 229–232; also Israel J. Tech., Vol. 23, 1986, pp. 141, 142. 4Rodden,W. P., Giesing, J. P., and Kalman, T. P., “Re nement of theNonPlanar Aspects of the Subsonic Doublet-Lattice Lifting Surface Method,” Journal of Aircraft, Vol. 9, No. 1, 1972, pp. 69–73. 5Rodden,W. P., Taylor, P. F., andMcIntosh,S. C., Jr., “FurtherRe nement of the Nonplanar Aspects of the Subsonic Doublet-Lattice Lifting Surface Method,”InternationalCouncilof theAeronautical Sciences, Paper 96-2.8.2, Sept. 1996. 6Dusto, A. R., et al., “AMethod for Predicting the StabilityDerivatives of an Elastic Airplane; Vol. I—FLEXSTAB Theoretical Description,” NASA CR-114712, Oct. 1974; also Air Force Flight Dynamics Lab., TR-74-91, Vol. 1, Nov. 1974. 7Rodden,W. P., and Johnson,E. H.,MSC/NASTRANAeroelastic Analysis User’s Guide, MacNeal-Schwendler Corp., 1994." @default.
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- W1990888046 title "Numerical Analysis of a Finite Wing Altered by a Leading-Edge Ice Accretion" @default.
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