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	Issue Date	Title	Author(s)
121	2001	Prediction of non-linear aeroelastic behaviour using normal form theory	Leung, Andrew Yee Tak
122	2000	Limit cycle oscillation prediction for non-linear aeroelastic systems with oscillatory aerodynamics	Leung, Andrew Yee Tak
123	2001	A finite element / modal technique for nonlinear plate and stiffened panel response prediction	Leung, Andrew Yee Tak
124	2000	Use of normal form theory to predict non-linear aeroelastic phenomena	Leung, Andrew Yee Tak
125	2000	Limit cycle oscillation prediction for aeroelastic systems with continuous non-linearities	Leung, Andrew Yee Tak
126	1999	Linear flutter prediction using symbolic programming	Leung, Andrew Yee Tak
127	1999	Simplified finite element modal model for non-linear beam response	Leung, Andrew Yee Tak
128	2002	Limit-cycle oscillation prediction for non-linear aeroelastic systems	Leung, Andrew Yee Tak
129	2000	Modelling of non-linear aerodynamics during limit cycle oscillations	Leung, Andrew Yee Tak
130	1999	A combined modal / finite element analysis technique for non-linear beam dynamic response under harmonic excitation	Leung, Andrew Yee Tak
131	2001	Non-linear random response of stiffened aerospace panels using a combined finite element / modal technique	Leung, Andrew Yee Tak
132	2001	A finite element / modal technique for nonlinear plate and stiffened panel response prediction	Leung, Andrew Yee Tak
133	2003	Curve fitting approach for transonic flutter prediction	Leung, Andrew Yee Tak
134	1999	A comparison of blade tip-timing data analysis methods	Leung, Andrew Yee Tak
135	2000	Prediction of non-linear aeroelastic instabilities	Leung, Andrew Yee Tak
136	2001	Estimation of the Hopf bifurcation point for aeroelastic systems	Leung, Andrew Yee Tak

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