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GoR Aerodynamics
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AG Nš
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TITLE
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Years
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AG01
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Wing/body aerodynamics
at transonic speeds
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1980-1984
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AG02
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Two-dimensional
transonic testing methods
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1980-1984
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AG03
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High lift, phase I
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1981-1984
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AG04
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Vortex flow
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1981-1984
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AG05
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Convergence study of
transonic flow computations for 3D wings
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1984-1987
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AG06
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Model support
interference in large low speed wind tunnels
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1984-1989
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AG07
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Experimental
investigation of the turbulent shear layer of a swept wing
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1986-1996
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AG08
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High lift, phase II
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1985-1990
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AG09
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Flow past missile
afterbodies
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1986-1991
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AG10
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Propeller performance
calculations
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1987-1990
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AG11
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Computations of 2D
Navier-Stokes equations
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1989-1995
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AG12
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Aeroacoustics for
propellers
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1991-1993
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AG13
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High lift, phase III
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1991-1994
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AG14
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Transition on
airfoils and infinite swept wings
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1991-1994
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AG15
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Validation of Euler
codes for supersonic flow
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1990-1995
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AG16
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Development of a
software package for graphic visualisation of flow simulation
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1991-1995
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AG17
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The verification of
3D transonic Euler methods for complex geometries
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1993-1996
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AG18
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Relative merits of
adaptive flexible wall test-sections
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1993-2003
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AG19
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Applicability of PIV
to large scale wind tunnels
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1994-1996
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AG20
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Mesh adaptation
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1995-1998
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AG21
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Pressure sensitive
paint
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1995-1998
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AG22
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Practical application
of LDV
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1995-1999
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AG23
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Three-dimensional
turbulent shear layer experiment, phase II
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1995-1998
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AG24
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Navier-Stokes calculations of the
supersonic flow about slender configurations
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1995-2003
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AG25
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High lift, phase IV
(maximum lift prediction)
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1995-1998
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AG26
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Transonic
wing/body Navier-Stokes computations
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1995-2001
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AG27
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Transition from
laminar to turbulent flows
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1996-1999
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AG28
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Transonic wing/body code validation
experiment
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1997-2004
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AG29
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Three-dimensional
shear layer experiment, phase III
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1999-2003
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AG30
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Supersonic Civil Transport low speed performance
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1999-2002
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AG31
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Drag extraction
for Supersonic Civil Transports
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1999-2001
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AG32
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Prediction of
performance degradation due to icing for 2D configurations
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1999-2003
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AG33
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Ice accretion
prediction on aircraft components
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1999-2003
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AG34
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Aerodynamics of supersonic air intakes
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1999-2006
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AG35
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Application of transition criteria in Navier-Stokes
computations
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1999-2002
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AG36
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Three-dimensional high lift computations
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1999-2004
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AG37
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Pressure sensitive paint, phase II
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2001-2004
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AG38
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Time accurate methods
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2001-2006
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AG39
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RANS code validation
for transonic wing-body, phase II
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2004-
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AG40
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Ice shape effects on
the aerodynamic performance of airfoils, phase II
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2004-
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AG41
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Ice accretion
prediction, phase II
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2004-
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AG42
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Navier-Stokes computations
of the transonic flow over slender configurations
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2005-
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AG43
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Application of CFD to
high offset intake diffusers
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2005-
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AG44
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Application of
transition criteria in Navier-Stokes computations, phase II
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2006-
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