72 wing flap combinations, including two aspect ratios, four taper ratios, and nine flap lengths are included in tables; comparisons between theoretical and experimental results for wings indicate that theory may be used to predict load distribution with sufficient accuracy for structural purposes.
Span load distribution for tapered wings with partial-span flaps
Nat Advisory Committee Aeronautics -- 23rd Annual Report
1937
18 pages
Bibliography
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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
|Calculation of aerodynamic characteristics of tapered wings with partial-span flaps
Engineering Index Backfile | 1939
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