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An aeroelastic model is constructed using the Rayleigh Ritz technique coupled with modified strip theory aerodynamics.
A new aerodynamic model is proposed based on modified strip theory (MST).
To model the complex aerodynamics of flapping-wing, an improved version of modified strip theory was chosen.
The modified strip theory is hence suggested as a general and effective steady aerodynamic tool for the multidisciplinary design and optimisation of flexible wings in the subsonic regime.
A Rayleigh Ritz type approach is used to model the aeroelastic behaviour of a simple rectangular unswept composite wing combined with modified strip theory aerodynamics.
The use of this modified strip theory is beneficial because it includes the unsteady aerodynamic effects and the possible change in the wings' dimensions.
Similar(53)
A partially body nonlinear time domain code based on strip theory is modified to include the surge mode.
The linear ship response in waves is evaluated using strip theory.
Wave loading is computed using Morisons equation in collaboration with the strip theory.
Additionally, the seakeeping trial results are used to validate a strip theory ship motion code.
For verification, the predicted results are compared with the experimental results and the strip theory results.
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