| 1210 |
 A method of estimating a separation boundary for two-dimensional aerofoil sections in transonic flow. |
81020 |
| 1210 |
The lift achievable by aerofoils having a particular form of supercritical upper-surface pressure distribution that yields only small wave drag. |
78010 |
| 1210 |
Aerofoils having a specified form of upper-surface pressure distribution: details and comments on design. |
71020 |
| 1210 |
Drag-rise Mach number of aerofoils having a specified form of upper-surface pressure distribution: charts and comments on design. |
71019 |
| 1210 |
A method of estimating drag-rise Mach number for two-dimensional aerofoil sections. |
TD MEMO 6407 |
| 1210 |
Methods for estimating the pressure distribution on a two-dimensional aerofoil in viscous transonic flow. |
81019 |
| 1210 |
Numerical methods for solving the potential flow equations for two-dimensional aerofoils in subsonic and transonic flows: brief details, test cases and examples. |
79009 |
| 1210 |
First-order method for estimating the subcritical pressure distribution on a two-dimensional aerofoil in compressible viscous flow. |
76002 |
| 1210 |
Second-order method for estimating the subcritical pressure distribution on a two-dimensional aerofoil in compressible inviscid flow. |
72025 |
| 1210 |
A method for estimating the pressure distribution on the surface of a two-dimensional aerofoil in a sonic stream. |
69013 |
