A procedure to simultaneously solve the Navier-Stokes equations and modal structural equations of motion is presented for computing aeroelastic responses of wings. The Navier-Stokes flow equations are solved by a finite-difference scheme with dynamic grids. The coupled aeroelastic equations of motion are solved using the linear acceleration method. The aeroelastic, configuration-adaptive dynamic grids are time accurately generated using the aeroelastically deformed shape of the wing. The unsteady flow calculations are validated with the experiment. Present development is demonstrated for computing vortical flows over flexible wings.
Numerical simulation of vortical flows on flexible wings
Numerische Simulierung von Wirbelstroemungen an flexiblen Tragflaechen
AIAA-Papers ; Jan ; 1-9
1988
9 Seiten, 9 Bilder, 16 Quellen
Conference paper
English
Numerical simulation of vortical flows on flexible wings
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