Simulation results of various NACA airfoil shapes and flow conditions for ML training.
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Plain Text - 754.9 MB - MD5: a040180be598dd385c58579d0e4c1361
Race CarRaw
Unknown - 6.0 GB - MD5: 1db0c9f71c379ad6fe54420c884b4990
DataRaw
Dataset for single-inverted airfoil with ground effect
Shell Script - 653 B - MD5: 069ac29c143a5a7b10fa81bcca534c9d
CodeCruise AOA=0Documentation
Linux script to restore Cruise AOA=0 OpenFOAM simulation cases
Shell Script - 628 B - MD5: 996d832c7d760e073c20846b965ea095
CodeCruise AOA=5Documentation
Shell Script - 596 B - MD5: 7eab389debed8913ae97acc31fe56d5f
CodeCruise RandomDocumentation
Shell Script - 598 B - MD5: 93e69bcf67e041f3f09eb3a7ddb23f04
CodeDocumentationRace Car
Shell Script - 595 B - MD5: bf602428cc92ddcfcdb1ae2f53f6f2c8
CodeCruise RandomDocumentation
Shell Script - 610 B - MD5: 6ec487eb45719a4917deee74852934ff
CodeCruise AOA=0Documentation
Shell Script - 612 B - MD5: 4a174661a12aaa1c812d8a5ee1ba714f
CodeCruise AOA=5Documentation
Shell Script - 622 B - MD5: 774ba68a76bea841cbb6095effd9d9ff
CodeDocumentationTakeoff
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