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Wind-tunnel research comparing lateral control devices, particularly at high angles of attack III : ordinary ailerons rigged up 10 degrees when neutral (1933)

NASA Technical Reports Server (NTRS) · leaf 5

An illustration from Wind-tunnel research comparing lateral control devices, particularly at high angles of attack III : ordinary ailerons rigged up 10 degrees when neutral, 1933, leaf 5
ith the type of airplane that is being considered. At a=30°, all of the ailerons gave very unsatis- For a highly maneuverable military or acrobatic factory control. machine, complete independence of the controls as lateral control with sideslip.—If a wing is yawed they affect the turning moments… … O 10' 20' 30' 40' covers the entire range that can be maintained in glides with most present-day conventional airplanes, Fiouee 6.—Boning criterion. -40 per cent chord by 30 per cent semlspan ailerons with various movements. (Neutral position 10° up) no adverse yawing moments were given by the…

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