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CFD simulation of a diamond airfoil (chord=2m, half-angle=12°) at Mach 1.6 and P=60kPa for angles of attack 0° to 5°.
by slilbaekslilbaek
saeedrz created this project
about 2 months ago
CFD simulation of a diamond airfoil (chord=2m, half-angle=12°) at Mach 1.6 and P=60kPa for angles of attack 0° to 5°.