60 |
Wave drag of flat plates with blunt noses at zero incidence. |
Aero W.S.02.03.10 |
60 |
Base pressure on aerofoil sections with a blunt trailing edge in supersonic flow. |
Aero W.S.02.03.07 |
60 |
The calculation of the theoretical characteristics of two-dimensional aerofoils at supersonic speeds. |
Aero W.S.00.03.05 |
60 |
Theoretical properties of two-dimensional supersonic aerofoils of simple section. |
Aero W.S.00.03.04 |
60 |
Introductory Item on two-dimensional aerofoils at supersonic speeds. |
AERO W.S.00.03.03 |
60 |
Aerofoil profile drag for Mach numbers below the drag rise condition.
show data item
|
00027 |
60 |
Profile drag at the drag-rise condition of aerofoils having a specified form of upper-surface pressure distribution at this condition. |
67011 |
60 |
Limit of surface waviness for laminar flow over wings. |
Aero W.02.04.11 |
60 |
Limit of grain size for laminar flow over wings or bodies. |
Aero W.02.04.09 |
60 |
Profile drag of smooth aerofoils with straight trailing- edges at low speeds. |
AERO W.02.04.03 |