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DCC Bridge
Anonymous1778856193
05-26 14:45
Model Name
turbine blade 3d model
Tags
machine
simulation
realistic
Prompt
NASA Rotor 67 transonic axial compressor rotor blade. Single blade, no hub or casing. The blade is a 3D twisted airfoil with 22 blades total on the original rotor. Key geometry: hub-to-tip ratio 0.375, blade chord ~3cm at hub increasing to ~5cm at tip, significant twist from hub to tip (~60 degrees total twist). The blade has a thin, cambered cross-section similar to a controlled-diffusion airfoil. Leading edge is sharp and rounded, trailing edge is thin. The blade leans slightly in the tangential direction. Span height approximately 6cm. The pressure side is slightly convex, suction side is more curved with higher camber. Smooth metallic surface, titanium alloy appearance, polished finish. No filleting at root. Isolated single blade shown at slight angle to reveal both pressure and suction surfaces and the twist along the span.
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