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DaleKramerUnited States
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DaleKramer's profile
eLazair4 - Real Life vs CFD
For Help - extractor mod curve - Copy
FOR HELP L_Cylinder_D_200mm_L_1m
Pontoons
EyePressFEA-NonLinear
FlatBottom
Mentor XS Paraglider
LazairFoil
WIP - vLazair
CyberTruck Geometry by DaleKramer
UNFINISHED-PressFEA-NonLinear
2019 vs 2020 TET meshes NACA0012
NACA0012 - - - - Verification using TETforCFD meshes
MESH ERROR - floating point exception
FORHELP-RadOn0p484375mGRID
UNFINISHED2 CyberTruck by Dale Kramer
TOPLAY-geometry import issue
PLAY-FeatureTest
UNFINISHED - Canard-vlb Dales Optimization Method
UNFINISHED-XFLR5vsCFD
UNFINISHED-8m Airship envelope
UNFINISHED-Airship p4H2O
PLAY-Silicone pocket
UNFINISHED-Filling a pillow cavity from a plastic extrusion nozzle
How to obtain Force Results that are rotated by the angle of the Inlet air, so that they represent true Lift and Drag values
UNFINISHED-8m Airship
PLAY-Water Rotor 1
UNFINISHED-GasBag
TOHELP-tcc_rodolfo - Dale1
TOHELP-Dale copy 6:31pm 4/14/19 Thrush S2R Lateral Stability, MK3
Retsam Pandora Box - Dale continuation
DaleKramer - SimWing Optimization Challenge
FEA von Mises Stress results versus Maximum Tet Edge Ratio of a mesh and of using SimScale Bonded Contact Study
1 boundary layer vs 3 layers HEX mesh Test at strict yPlus20-175
UNFINISHED 2s - Mentor XS Paraglider Root Airfoil
UNFINISHED - Drafting Ahmed Bodies
'TETforCFD' meshes using 'new mesh preview' algorithm meshes - Finding Numerics to obtain efficient and stable Convergence for CFD
01234 layer HEX mesh Test
yPlusHisto mesh RW2-1.3
UNFINISIHED level0 BMB grid alignment study
FORHELP UrbanWind
yPlus - Metrics to evaluate yPlus achieved in CFD Boundary Layer Analysis
MESH ERROR OK but not perfect SOLUTION - floating point exception
CyberTruck Geometry by DaleKramer
yPlus - Strict yPlus ranging for CFD Boundary Layer Analysis
TETforCFD Residual Investigation
Sphere 2687mm
FORHELP_FSAE Rear wing mesh study
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