naca-tn-614
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National Advisory Committee for Aeronautics, Technical Notes - Fuselage Drag Tests in the Variable Density Wind Tunnel; Streamline Bodies of Revolution, Fineness Ratio of 5
| File | Action |
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| naca-tn-614 Fuselage Drag Tests in the Variable Density Wind Tunnel; Streamline Bodies of Revolution, Fineness Ratio of 5.pdf | Download |
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