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A.1) Structured multi-block grid
around a complete
transport aircraft (Euler grid)
A.2) Unstructured hybrid grid around
a complete
transport aircraft (RANS grid)
A.3) Unstructured hybrid grid around
a bridge deck
section (for RANS computation)
A.4) Grid adaptation (symmetrical
aerofoil in a
transonic flow with a shock wave)
A.5) Grid convergence study
(transonic flow around
a supercritical aerofoil)
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B.1) Influence of turbulence
modelling (symmetrical
aerofoil in steady transonic flow)
B.2) Influence of turbulence
modelling (unsteady
flow around a bridge deck section)
B.3) Detached-Eddy Simulation (DES)
vs. Unsteady
Reynolds-Averaged Navier-Stokes (URANS)
approach (flow around a
rectangular cylinder)
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C.1) Engine-airframe aerodynamic
interaction for a
transport aircraft
C.2) Influence of Gurney flap on
aerofoil’s performance
C.3) Unsteady interaction between shock wave and
boundary layer (self-induced shock oscillation +
detachment of large eddies)
C.4) Aerofoil trailing edge as an
acoustic source
(transonic flow with self-induced shock motion
and
alternating boundary layer separation)
C.5) Bluff-body aerodynamics - influence of body
length
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