NACA-TN-4341
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- March 24, 2016 Create Date
- March 24, 2016 Last Updated
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National Advisory Committee for Aeronautics, Report - Low-Speed Experimental Determination of the Effects of Leading-Edge Radius and Profile Thickness on Static and Oscillatory Lateral Stability Derivatives for a Delta Wing with 60° of Leading Edge Sweep
| File | Action |
|---|---|
| naca-tn-4341 Low-Speed Experimental Determination of the Effects of Leading-Edge Radius and Profile Thickness on Static and Oscillatory Lateral Stability Derivatives for a Delta Wing with 60°.pdf | Download |
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