naca-report-1167
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- November 2, 2016 Create Date
- November 2, 2016 Last Updated
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National Advisory Committee for Aeronautics, Report - Method for Calculating the Rolling and Yawing Moments Due to Rolling for Unswept Wings with or Without Flaps or Ailerons by Use of Nonlinear Section Lift Data
| File | Action |
|---|---|
| naca-report-1167 Method for Calculating the Rolling and Yawing Moments Due to Rolling for Unswept Wings with or Without Flaps or Ailerons by Use of Nonlinear Section Lift Data.pdf | Download |
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