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5 Geometries
5 Meshes
6 Simulation setups
9 ResultsThis project is intended to investigate the different drag characteristics of versions of fins intended for a model rocket using the Prandtl-D tip (NASA Preliminary Research Aerodynamic Design To Lower Drag) airfoil profile. The primary intent is to determine whether drag characteristics are improved or detracted by the truncation of the fin profile through the limitation of max thickness of the fin. - Copy
by simscalesimscale
5 Geometries 5 Meshes 6 Simulation setups 9 ResultsThis project is intended to investigate the different drag characteristics of versions of fins intended for a model rocket using the Prandtl-D tip (NASA Preliminary Research Aerodynamic Design To Lower Drag) airfoil profile. The primary intent is to determine whether drag characteristics are improved or detracted by the truncation of the fin profile through the limitation of max thickness of the fin. - Copy
notfeynman created this project
over 7 years ago
gprachi877 copied this project
15 days ago
