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A method for the active vibration suppression of a cantilever wing is presented.
A method for the prediction of the acoustics of a propeller in the flow-field of a wing is presented.
A model for sound generation by a jet in the vicinity of a flat plate, mimicking an exhaust jet installed near an aircraft wing, is presented.
A state-space reduced-order model for the lift generated by the unsteady deflection of a two-dimensional flexible wing is presented.
In our present study, evidence for neurogenesis in the adult Drosophila wing is presented.
On the basis of the artificial neural network approach, an optimization process of slat cove filler (SCF) for high lift devices (HLD) on the Trap Wing is presented.
Similar(54)
In this paper, high-order Discontinuous Galerkin (DG) Reynolds Averaged Navier Stokes (RANS) computations of the turbulent incompressible flow over a 65° deg sweep delta wing are presented.
Furthermore, experimental results on a fly wing are presented in the experiment section; and, finally, conclusions are drawn.
A semi-analytical model for the combined static aeroelastic analysis and response of flexible subsonic wings is presented.
Here, a review on the state-of-the-art on non-linear aeroelasticity of high aspect-ratio wings is presented.
The methodologies employed to analyse high aspect-ratio wings are presented and their applications discussed.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com