Investigations on a STOL-airplane with internally blown flaps are described. To avoid flow separation on the wing, slots were located behind the nose flap and in front of the trailing edge flap. Maximum lift and optimum L/D were investigated, as well as the effectiveness of the aileron and the horizontal tail. (Author)
Three Component Measurements on a Light STOL Aircraft with Chordwise Blowing
1975
23 pages
Report
Keine Angabe
Englisch