We shall attempt here to summarize the existing data on the values of the low-speed CLmax. of wings, in the absence of a fuselage, and without including information on stalling incidence or pitching moment. The summary is limited to the consideration of unswept wings, and those of delta plan form, which have symmetrical sections: there is some discussion of the maximum lift increments due to the use of flaps of various kinds.
Maximum Lift Data for Symmetrical Wings
A Resumé of Maximum Lift Data for Symmetrical Wings, including various High-Lift Aids
Aircraft Engineering and Aerospace Technology ; 27 , 1 ; 2-8
01.01.1955
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Maximum lift data for symmetrical wings
Engineering Index Backfile | 1955
|Maximum lift prediction for multielement wings
AIAA | 1992
|Maximum-lift and stalling characteristics of wings
NTRS | 1948
|Investigation of maximum lift of wings at supersonic speeds
Engineering Index Backfile | 1955
|