1230 |
Vortex generators for control of shock-induced separation. Part 3: examples of applications of vortex generators to aircraft. |
93026 |
1230 |
Vortex generators for control of shock-induced separation. Part 2: guide to use of vane vortex generators. |
93025 |
1230 |
Vortex generators for control of shock-induced separation. Part 1: introduction and aerodynamics. |
93024 |
1230 |
A method of estimating a flow breakdown boundary for aerofoils and swept wings in transonic flow. |
91021 |
1230 |
A method of determining the wave drag and its spanwise distribution on a finite wing in transonic flow. |
87003 |
1230 |
A framework relating the drag-rise characteristics of a finite wing/body combination to the those of its basic aerofoil. |
78009 |
1230 |
Adaptation of drag-rise charts in T.D. Memor. 71019 to the mid-semi-span portion of swept and tapered planforms. |
72027 |
1230 |
Method for predicting the pressure distribution on swept wings with subsonic attached flow. |
73012 |
1230 |
Method for the rapid estimation of theoretical spanwise loading due to a change of incidence. |
TD MEMO 6403 |
1230 |
Graphical method for estimating the spanwise distribution of aerodynamic centre on wings in subsonic flow. |
TD MEMO 6309 |