NASA NACA-RM-A8D02-1949
Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees - investigation of a large-scale model at low speed
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NASA NACA-RM-A8D02-1949
Standard No.
NASA NACA-RM-A8D02-1949
Release Date
1949
Published By
National Aeronautics and Space Administration (NASA)
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