1. Readers Forum
2. Readers Forum
3. Aerodynamic Influence Coefficients for an Oscillating Finite Thin Wing in Supersonic Flow
4. Stagnation Point of a Blunt Body in Hypersonic Flow
5. J. D. Murray, “The boundary layer on a flat plate when the main stream has uniform shear,” Division of Engineering and Applied Physics, Harvard University (June, 1958).