Lift, drag, and pitching moments were measured for wing with three different sizes of flap; it was found that any gap between flap and wing reduced lift, drag, and pitching moments, but that center-of-pressure movement and ratio of lift were little affected.
Wind-tunnel tests of clark Y wing having split flaps with gaps
Nat Advisory Committee Aeronautics -- Tech Note
1938
4 pages
3 Supp plates, Bibliography
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Wind-tunnel tests of clark Y wing having split flaps with gaps
Engineering Index Backfile | 1938
|Wind-tunnel tests of a Clark Y wing having split flaps with gaps
TIBKAT | 1938
|Effect of partial-span split flaps on aerodynamic characteristics of clark Y wing
Engineering Index Backfile | 1933
|