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Seriously
good AEROELASTIC Pre and Postprocessor:
AES=V=
- Warping &
Mollifying &
Gridgeneration,
- Flutter
& Time Trace Analysis
- Analysis and
comparison of calculated and experimental data.
- Data stored
in a simple format (files containing sheets of
tabular data.)
- Easy comparison of
data from various sources.
xy plots, quasi 3D plots, 3D projection
plots & OpenGL visualizations.
- Screen, postscript
&ppm
- Geometric Slicing
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AES=V=
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AES=3=
- Calculates 3D unsteady aerodynamic
forces&pressures on oscillating surfaces
using panel methods
- Incompressible, subsonic and supersonic/Hypersonic
- Piston theories implicit/explicit
accounting for thickness
- Propiertor nearly exact wedge
treatment
- Hypersonic
true surface modelling
- rigid, sub-rigid (effectors)
& arbitrary motions
- Warping
- Harmonic and exponentionally
growing unsteady motions are
modelled
- Pressure and generalised force
coefficients
- Data, xls and graphical output
- An
aero(-servo-)elastic design cycle
accelerator
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AES=3=
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AES=O=
- Prediction & analysis of 2D & 3D
steady & unsteady
aerodynamic/hydrodynamic
forces on
platforms (thick & flat surface panel
methods)
- Suction Force
modelling (correct induced drag on lifting
surfaces !!)
- Incompressible, subsonic (~transonic)
and supersonic
- Havelock
sources & doublets (implicit linearized
free-surface BC) for Froude >=0. and
frequency >=0.
- rigid, sub-rigid(effectors)
& arbitrary elastic motions
- Trim and boundary layer modelling
- Warping
- Free-surface
modelling (Rankine model)
- Acoustic
modelling
- Harmonic and exponentionally growing
unsteady motions
- Pressure and generalised force
coefficients
- Data, xls and graphical output
 
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AES=O=
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AES=2=
- Calculates 2D
unsteady aerodynamic
forces & pressures on (partly) oscillating
flat plates using panel methods in frequncy
domain
- Incompressible,
subsonic, sonic and
supersonic/Hypersonic
- Piston theories implicit/explicit
accounting for thickness
- Propiertor nearly exact wedge
treatment
- Pitching,
plunging
- Trailing edge
flap Pitch and Plunge
- Leading edge flap
Pitch and Plunge
- Mid chord flap
Pitch and Plunge
- Parabolic
displacement
- Sinusoidal
gust
- Arbitrary
motion
- Pressure,
force, moment and generalised force
coefficients
- Data, xls and
graphical output
- An
alternative & enrichment to AGARD VI
table look up
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AES=2=
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AES=W=
- Calculates 2D unsteady aerodynamic
forces & pressures on (partly) oscillating
flat plates using panel methods
- The flat plate is placed in between
upper and lower walls.
- The walls are modeled as closed, open or ventilated.
- Harmonic and exponentionally
growing unsteady motions are
modelled
- Incompressible & subsonic flow
- Pitching, plunging
- Trailing
edge flap Pitch and Plunge
- Leading
edge flap Pitch and Plunge
- Mid
chord flap Pitch and Plunge
- Parabolic displacement
- Sinusoidal gust
- Arbitrary motion
- Pressure, force, moment and generalised
force coefficients
- Data, xls and graphical output
- A wind tunnel
correction estimator
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AES=W=
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| © 2019
AES4AC |
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