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A comprehensive mechanical model based on the nonlinear large deflection beam theory for the deepwater SLWR transfer process is developed.
In this paper, a method is proposed for modelling large deflection beam response involving multiple vibration modes.
An aeroelastic analysis of bearingless rotors is investigated using large deflection beam theory in hover and forward flight.
Table 7 Beam collapse load and deflection Beam type Collapse load (kN) Deflection (mm) T-beam 41 15 Triangular I 34 18 Triangular II 45 24 Open image in new window Fig. 8 Beam load deflection response.
In this work, an analytical model of a 3D re-entrant honeycomb auxetic cellular structure has been established based on both a large deflection beam model and a Timoshenko beam model.
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Furthermore, based on small-deflection beam theory, the effect of a liquid droplet on the deflection of a MCL was also studied.
The compliant constant-force compression mechanism (CFCM) is a slider mechanism incorporating large-deflection beams, which outputs near-constant-force across the range of its designed deflection.
A methodology is based on the calculation of the deflection of beam on an elastic foundation from the deflection of a reference beam which is topologically equivalent.
Transverse deflection of beam.
The deflection of beam is analytically calculated.
Open image in new window Fig. 6 Location of points A and B. Table 6 Maximum deflection of beam.
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