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Issue DateTitleAuthor(s)
2012001A combined modal/finite element analysis technique for the dynamic response of a non-linear beam to harmonic excitationLeung, Andrew Yee Tak 
2022001Prediction of non-linear aeroelastic behaviour using normal form theoryLeung, Andrew Yee Tak 
2032000Limit cycle oscillation prediction for non-linear aeroelastic systems with oscillatory aerodynamicsLeung, Andrew Yee Tak 
2042000Finite element analysis of rubber mounts under shock loadingLeung, Andrew Yee Tak 
2052001A finite element / modal technique for nonlinear plate and stiffened panel response predictionLeung, Andrew Yee Tak 
2062000Use of normal form theory to predict non-linear aeroelastic phenomenaLeung, Andrew Yee Tak 
2072000Limit cycle oscillation prediction for aeroelastic systems with continuous non-linearitiesLeung, Andrew Yee Tak 
2081999Linear flutter prediction using symbolic programmingLeung, Andrew Yee Tak 
2091999Simplified finite element modal model for non-linear beam responseLeung, Andrew Yee Tak 
2102002Limit-cycle oscillation prediction for non-linear aeroelastic systemsLeung, Andrew Yee Tak 
2112000Modelling of non-linear aerodynamics during limit cycle oscillationsLeung, Andrew Yee Tak 
2121999A combined modal / finite element analysis technique for non-linear beam dynamic response under harmonic excitationLeung, Andrew Yee Tak 
2132001Non-linear random response of stiffened aerospace panels using a combined finite element / modal techniqueLeung, Andrew Yee Tak 
2142001A finite element / modal technique for nonlinear plate and stiffened panel response predictionLeung, Andrew Yee Tak 
2152003Curve fitting approach for transonic flutter predictionLeung, Andrew Yee Tak 
2161999A comparison of blade tip-timing data analysis methodsLeung, Andrew Yee Tak 
2172000Prediction of non-linear aeroelastic instabilitiesLeung, Andrew Yee Tak 
2182001Estimation of the Hopf bifurcation point for aeroelastic systemsLeung, Andrew Yee Tak 
Results 1-18 of 18 (Search time: 0.016 seconds).

 

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