Computational aerodynamic design of advanced fighter wings with well-controlled transonic maneuver flow and high supersonic cruise efficiency is described. (Author)
Supersonic Cruise/Transonic Maneuver Wing Section Development Study
1980
77 pages
Report
No indication
English
Aircraft , Aerodynamics , Aeronautics , Flight maneuvers , Transonic flight , Swept wings , Supersonic flight , Aerodynamic loading , Dual mode , Jet fighters , Level flight , Potential flow , Optimization , Supercritical flow , Camber , Variables , Aeroelasticity , Aspect ratio , Boundary layer , Aerodynamic drag , Canard configuration , Lift , Bias , Aerodynamic stability , Coefficients , Computer aided design , Trade off analysis , Cruising flight , Aeroelastic tailoring , Variable camber
LAMINAR FLOW WING OPTIMIZED FOR TRANSONIC AND SUPERSONIC CRUISE AIRCRAFT
European Patent Office | 2021
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