Investigations on a STOL aircraft with internally blown flaps are described. To avoid separation on the wing, slots were located behind the nose flap and in front of the trailing edge flap. The investigations were designed to examine maximum lift and lift/drag ratio. In addition, the effectiveness of the aileron and the horizontal tail were investigated. (Author)
Three-Component Measurements on a Model of a Light STOL Aircraft with Chordwise Blowing
1976
22 pages
Report
Keine Angabe
Englisch