Wind tunnel tests of effectiveness of methods of reducing high control forces of unbalanced upper-surface ailerons and of unbalanced split flaps; tests of aileron-axis and flap-axis locations and arrangements of aileron and flap slots, all on Clark Y wing; lift and drag characteristics of various arrangements. (Price 10c.)
Wind-tunnel investigation of aerodynamic balancing of upper-surface ailerons and split flaps
Nat Advisory Committee Aeronautics -- Report
1935
18 pages
Bibliography
Report
English
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Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Engineering Index Backfile | 1937
|Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Engineering Index Backfile | 1937
|Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Engineering Index Backfile | 1937
|