A method of providing an aircraft having a fuselage and a wing configured for extensive laminar flow at design cruise conditions, the method characterized by a) providing wing biconvex-type airfoils having values of thickness, chord and shape along the wing span which provide substantially optimal aircraft range at design cruise conditions, considering the influences of wing drag and wing weight; b) providing wing leading edges, which are configured to effect laminar flow; c) providing fuselage and wing contours which, in combination, produce reduced total wave drag and produce extensive areas of laminar boundary layer flow on the wing; and d) providing wing sweep angularity that facilitates provision of a), b) and c).
LAMINAR FLOW WING OPTIMIZED FOR SUPERSONIC AND HIGH SUBSONIC CRUISE AIRCRAFT
LAMINARFLUSSFLÜGEL FÜR MIT ÜBERSCHALL- UND HOHER UNTERSCHALLGESCHWINDIGKEIT FLIEGENDE FLUGZEUGE
AILE À ÉCOULEMENT LAMINAIRE OPTIMISÉE POUR AÉRONEF À VITESSE DE CROISIÈRE SUPERSONIQUE ET SUBSONIQUE
2015-09-23
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
LAMINAR FLOW WING OPTIMIZED FOR SUPERSONIC AND HIGH SUBSONIC CRUISE AIRCRAFT
Europäisches Patentamt | 2018
|LAMINAR FLOW WING OPTIMIZED FOR SUPERSONIC AND HIGH SUBSONIC CRUISE AIRCRAFT
Europäisches Patentamt | 2015
|LAMINAR FLOW WING OPTIMIZED FOR TRANSONIC AND SUPERSONIC CRUISE AIRCRAFT
Europäisches Patentamt | 2021
|