The development of four wings which were designed to have specific aerodynamic requirements is described. The wings designed were: a high lift wing, a low lift or cruise wing, both of which were smooth, and two flapped wings which were approximations of the smooth wings.
High Lift Surface Design Procedures. Experimental Verification. Volume II. Theoretical Design and Analysis
1966
2 pages
Report
No indication
English
STOL High-Lift Design Study. Volume II. Bibliography
NTIS | 1971
|CD volume design and verification
AIAA | 1993
|High lift airfoil design method, high lift airfoil and aircraft
European Patent Office | 2023
|