Measured And Predicted Section Wave Drag Coefficients At A Mach Number Of 16 For A Delta Wing With Two Airfoil Sections
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Measured and Predicted Section Wave Drag Coefficients at a Mach Number of 1.6 for a Delta Wing with Two Airfoil Sections
| Author | : Frederick C. Grant |
| Publisher | : |
| Total Pages | : 46 |
| Release | : 1959 |
| Genre | : Mach number |
| ISBN | : |
NASA Technical Note
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 910 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
Index of NACA Technical Publications
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 860 |
| Release | : 1957 |
| Genre | : Aeronautics |
| ISBN | : |
A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0
| Author | : Robert S. Osborne |
| Publisher | : |
| Total Pages | : 20 |
| Release | : 1960 |
| Genre | : Aerodynamics |
| ISBN | : |
Index of NASA Technical Publications
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 448 |
| Release | : 1960 |
| Genre | : Aeronautics |
| ISBN | : |
Index to NASA Technical Publications
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : |
| Release | : 1960-07 |
| Genre | : |
| ISBN | : |
