28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-2.11.2
SMALL DISTURBANCE NAVIER-STOKES INVESTIGATIONS OF FIGHTER-TYPE-DELTA-WING PITCHING OSCILLATIONS
TU Munich, Germany
Keywords: small disturbance navier-stokes equations, computational fluid dynamics, aeroelasticity
For transonic production aeroelastic analysis the small disturbance Navier-Stokes method FLM-SD.NS was shown to be an efficient and yet accurate alternative to the corresponding dynamically fully nonlinear Reynolds-averaged Navier-Stokes method. FLM-SD.NS is employed to novelly investigate unsteady aerodynamic cases of a fighter-type delta-wing performing harmonic pitching oscillations.
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