Results of flight tests on low-wing monoplane; leading-edge slots over entire wing and flaps extending to ailerons increase lift 94 per cent, increase glide angle 4.2 deg.; span, 35 ft.; weight 1800 lb.; 16.3 lb. per hp.; 9.1 lb. per sq. ft. Warner Scarab, 110 hp. at 1850 r.p.m.
Effect of slots and flaps on lift and drag of McDonnell airplane as determined in flight
Nat. Advisory Committee Aeronautics -- Tech. Notes
1931
12 pages
15 Figs., Supp. plates
Report
Englisch
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Flaps, Slots and Other High Lift Aids
Emerald Group Publishing | 1955
|Flaps, slots and other high lift aids
Engineering Index Backfile | 1955
|