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	Issue Date	Title	Author(s)
1	2001	Prediction of non-linear aeroelastic behaviour using normal form theory	Leung, Andrew Yee Tak
2	2000	Limit cycle oscillation prediction for non-linear aeroelastic systems with oscillatory aerodynamics	Leung, Andrew Yee Tak
3	2001	A finite element / modal technique for nonlinear plate and stiffened panel response prediction	Leung, Andrew Yee Tak
4	2000	Use of normal form theory to predict non-linear aeroelastic phenomena	Leung, Andrew Yee Tak
5	2000	Limit cycle oscillation prediction for aeroelastic systems with continuous non-linearities	Leung, Andrew Yee Tak
6	1999	Linear flutter prediction using symbolic programming	Leung, Andrew Yee Tak
7	1999	Simplified finite element modal model for non-linear beam response	Leung, Andrew Yee Tak
8	2002	Limit-cycle oscillation prediction for non-linear aeroelastic systems	Leung, Andrew Yee Tak
9	2000	Modelling of non-linear aerodynamics during limit cycle oscillations	Leung, Andrew Yee Tak
10	1999	A combined modal / finite element analysis technique for non-linear beam dynamic response under harmonic excitation	Leung, Andrew Yee Tak
11	2001	Non-linear random response of stiffened aerospace panels using a combined finite element / modal technique	Leung, Andrew Yee Tak
12	2001	A finite element / modal technique for nonlinear plate and stiffened panel response prediction	Leung, Andrew Yee Tak
13	2003	Curve fitting approach for transonic flutter prediction	Leung, Andrew Yee Tak
14	1999	A comparison of blade tip-timing data analysis methods	Leung, Andrew Yee Tak
15	2000	Prediction of non-linear aeroelastic instabilities	Leung, Andrew Yee Tak
16	2001	Estimation of the Hopf bifurcation point for aeroelastic systems	Leung, Andrew Yee Tak

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