A pre-World War 2 German patent is described for an airplane wing whose profile is automatically changed as a function of the flight parameters (velocity, angle of attack, etc.) in such a manner that the center of pressure always remains approximately at the same place. The patent includes an automatic steering device for aircraft. Conventional and wing-only aircraft are considered. (Author)
Lifting Surface for Aircraft
1975
22 pages
Report
Keine Angabe
Englisch
AIRCRAFT LIFTING SURFACE AND AIRCRAFT COMPRISING SUCH LIFTING SURFACE
Europäisches Patentamt | 2024
|AIRCRAFT LIFTING SURFACE AND AIRCRAFT COMPRISING SUCH LIFTING SURFACE
Europäisches Patentamt | 2024
|