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Title
Author(s)
41
2001
Prediction of non-linear aeroelastic behaviour using normal form theory
Leung, Andrew Yee Tak
42
2000
Limit cycle oscillation prediction for non-linear aeroelastic systems with oscillatory aerodynamics
Leung, Andrew Yee Tak
43
2001
A finite element / modal technique for nonlinear plate and stiffened panel response prediction
Leung, Andrew Yee Tak
44
2000
Use of normal form theory to predict non-linear aeroelastic phenomena
Leung, Andrew Yee Tak
45
2000
Limit cycle oscillation prediction for aeroelastic systems with continuous non-linearities
Leung, Andrew Yee Tak
46
1999
Linear flutter prediction using symbolic programming
Leung, Andrew Yee Tak
47
1999
Simplified finite element modal model for non-linear beam response
Leung, Andrew Yee Tak
48
2002
Limit-cycle oscillation prediction for non-linear aeroelastic systems
Leung, Andrew Yee Tak
49
2000
Modelling of non-linear aerodynamics during limit cycle oscillations
Leung, Andrew Yee Tak
50
1999
A combined modal / finite element analysis technique for non-linear beam dynamic response under harmonic excitation
Leung, Andrew Yee Tak
51
2001
Non-linear random response of stiffened aerospace panels using a combined finite element / modal technique
Leung, Andrew Yee Tak
52
2001
A finite element / modal technique for nonlinear plate and stiffened panel response prediction
Leung, Andrew Yee Tak
53
2003
Curve fitting approach for transonic flutter prediction
Leung, Andrew Yee Tak
54
1999
A comparison of blade tip-timing data analysis methods
Leung, Andrew Yee Tak
55
2000
Prediction of non-linear aeroelastic instabilities
Leung, Andrew Yee Tak
56
2001
Estimation of the Hopf bifurcation point for aeroelastic systems
Leung, Andrew Yee Tak
Results 1-16 of 16 (Search time: 0.017 seconds).
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Sedaghat, A.
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McEwan, M. I.
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Carrington, I. B.
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Sedhaghat, A.
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Vio, G.