Aircraft Stability Analysis Including Unsteady Aerodynamic Effects

123[10] Jones, R. T., “The Unsteady Lift of a Wing of Finite Aspect Ratio”, NACARep. 681, June 1939.[11] Jones, R. T., “The Unsteady Lift of a Finite Wing”, NACA TN 682,Washington, D.C., January 1939.[12] Jones, R. T., Fehlner, L. F., “Transient Effects of the Wing Wake on theHorizontal Tail”, NACA TN 771, 1940.[13] Tobak, M., “On the Use of the Indicial Function Concept in the Analysis ofUnsteady Motions of Wings and Wing-Tail Combinations”, NACA Report1188, 1954.[14] Tobak, M., and Pearson, W. E., “A Study of Nonlinear LongitudinalDynamic Stability”, NASA TR R-209, September 1964.[15] Tobak, M., and Schiff, L. B., “On the Formulation of the AerodynamicCharacteristics in Aircraft Dynamics”, NASA TR-R-456, 1976.[16] Tobak, M., Chapman, G. T., Schiff, L. B., “Mathematical Modeling of theAerodynamic Characteristics in Flight Dynamics”. NASA TM-85880, Jan.1984.[17] Tobak, M., Chapman, G. T., “Nonlinear Problems in Flight DynamicsInvolving Aerodynamic Bifurcations”, NASA-TM-86706, March 1985.[18] Klein, V., and Noderer, K. D., “Modeling of Aircraft Unsteady AerodynamicCharacteristics, Part 1 – Postulated Models”, NASA TM 109120, May 1994.