Factors derived from wing theory presented; by means of these factors, angle of zero lift, lift curve slope, pitching moment, aerodynamic center position, and induced drag of tapered wings with partial span flaps may be calculated; factors given for wings of aspect ratios 6 and 10, of taper ratios from 0.25 to 1.00, and with flaps of various lengths. (10¢)
Calculation of aerodynamic characteristics of tapered wings with partial-span flaps
Nat Advisory Committee Aeronautics -- Report
1939
18 pages
Report
Englisch
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Span load distribution for tapered wings with partial-span flaps
Engineering Index Backfile | 1937
|Span load distribution for tapered wings with partial-span flaps
Engineering Index Backfile | 1937
|Span load distribution for tapered wings with partial-span flaps
TIBKAT | 1937
|