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CFD AES=4= solution Mach Number=10
In particular flutter support based on advanced panel methods and
on linear and nonlinear unsteady CFD methodology (Full Potential, Euler, Reynolds Averaged Navier Stokes(URANS), Thin Layer Reynolds Averaged Navier Stokes(TLNS), Baldwin Lomax and Spalart Allmaras turbulence models). True surface and transpiration boundary conditions.
AES4AC can perform very fast and efficient A/C flutter analysis and calculation of generalised airforces by means of its aero-elastic workbench importing generalised mass, stiffness, node coordinates and mode shapes obtained from FEM applications.
(hinfo@aes4ac.com)
AES4AC assistance, apps, codes, training & user support can be obtained from AES4AC hinfo@aes4ac.com           |
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