200 |
Drag of two-dimensional steps and ridges immersed in a turbulent boundary layer for Mach numbers up to 3. |
75031 |
200 |
Drag due to grooves in a flat plate with a turbulent boundary layer, at subsonic and supersonic speeds. |
75028 |
200 |
Drag due to a circular cavity in a plate with a turbulent boundary layer at subsonic, transonic and supersonic speeds. |
74036 |
200 |
Approximate wave drag of rectangular planform fairings at zero incidence in supersonic flow. |
71018 |
200 |
An introduction to aircraft excrescence drag. |
90029 |
200 |
Low-speed drag coefficient increment at constant lift due to full-span plain flaps. |
87024 |
200 |
Increment in aerofoil profile drag coefficient due to the deployment of a single-slotted flap. |
87005 |
200 |
Low-speed drag coefficient increment at zero lift due to full-span split flaps. |
74010 |
200 |
Vortex drag coefficient of wing with part-span flap and central cut-out. |
Aero F.02.01.08 |
200 |
Conversion factor for profile drag increment for part-span flaps. |
Aero F.02.01.07 |