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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
aes=o=: 3D advanced panelmethod for incompressible, subsonic and supersonic/Hypersonic flow about realistic thick bodies. Free surface and acoustic modelling.
aes=v=: Warping & Mollifying & surface design & mesh generation, Flutter & Time Trace Analysis & MIMO model generation

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 and on linear and nonlinear unsteady CFD methodology(AES=4=)

Downloads

hinfo@aes4ac.co

Publications