AES4AC HOME

Michael H. L. Hounjet, CEO

AES4AC has developed software/apps dealing with aeroelastic modelling in Subsonic, Transonic, Supersonic and Hypersonic operations.

The apps collection which can be obtained from AES4AC is:

aes=2= :An alternative & enrichment to AGARD VI table look up, Calculates 2D unsteady sectional aerodynamic forces & pressures on (partly) oscillating flat plates using panel methods in frequency domain in Incompressible, subsonic, sonic and supersonic/Hypersonic flow
aes=w=: A wind tunnel correction estimator Calculates 2D unsteady aerodynamic forces & pressures on (partly) oscillating flat plates in subsonic flow between upper and lower walls.modeled as closed, open or ventilated.
aes=3=: 3D advanced panelmethod for incompressible, subsonic and supersonic/Hypersonic flow about thin lifting surfaces. An aero(-servo-)elastic design cycle accelerator. Includes warping and H method.
aes=o= :3D advanced panelmethod for incompressible, subsonic and supersonic/Hypersonic flow about realistic thick bodies. Free surface and acoustic modelling. Includes warping and H method.
aes=v= : The Aeroelastic Pre and Postprocessor: Warping & Mollifying & surface design & mesh generation, Flutter & Time Trace Analysis & MIMO model generation. H flutter and GAF generation from time traces.

Linear Workflow for AES=3=/AES=O= and
AES=V=

AES4AC can be hired to provide expert assistance/second opinions in aeroelasticity and flutter speed prediction for Subsonic, Transonic, Supersonic and Hypersonic operations using its aero-elastic workbench importing generalised mass, stiffness, node coordinates and mode shapes obtained from FEM applications and calculation of generalised airforces by means of its advanced panel methods (aes=3= & aes=o=) and on linear and nonlinear unsteady CFD methodology( aes=4=: )

Downloads

hinfo@aes4ac.com

Publications

aes=2= :An alternative & enrichment to AGARD VI table look up, Calculates 2D unsteady sectional aerodynamic forces & pressures on (partly) oscillating flat plates using panel methods in frequency domain in Incompressible, subsonic, sonic and supersonic/Hypersonic flow

aes=w=: A wind tunnel correction estimator Calculates 2D unsteady aerodynamic forces & pressures on (partly) oscillating flat plates in subsonic flow between upper and lower walls.modeled as closed, open or ventilated.

aes=3=: 3D advanced panelmethod for incompressible, subsonic and supersonic/Hypersonic flow about thin lifting surfaces. An aero(-servo-)elastic design cycle accelerator. Includes warping and H method.

aes=o= :3D advanced panelmethod for incompressible, subsonic and supersonic/Hypersonic flow about realistic thick bodies. Free surface and acoustic modelling. Includes warping and H method.

aes=v= : The Aeroelastic Pre and Postprocessor: Warping & Mollifying & surface design & mesh generation, Flutter & Time Trace Analysis & MIMO model generation. H flutter and GAF generation from time traces.