1. Some Ballistic Contributions to Aerodynamics
2. I n view of experimental data that I have obtained subsequent to the writing of my article, it is my opinion that the above 1 I I t 1 • 1 I 1 I -4-1 I 1 . I \ 50 AO 3 0 1Q \0 O \0 2 0
3. Mathews, Charles W., and Thompson, Jim Rogers, Free-Fall Measurements at Transonic Velocities of the Drag of a Wing-Body Configuration Consisting of a 45° Swept-Back Wing Mounted Forward of the Maximum Diameter on a Body of Fineness Ratio 12, National Advisory Committee for Aeronautics, R.M. No. L6L26.
4. Shock-Wave Oscillations in Wind Tunnels