The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel data (1937)
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s (reference 7). The control devices have been used as checks of the com- wind-tunnel program included experiments to deter- putations. These tests were conducted by gliding the mine several important lateral-stability characteristics airplane at various steady speeds and suddenly deflect- as well… … Time, seconds Time, seconds Figure 1.—Boiling and yawing motion of F-22 airplane with long narrow ailerons. Fioube 3.—EoMng and yawing motion ol F-22 airplane with balanced short wide Flaps up; Cl°U ailerons. Flaps np; OvlJO .8 8 U Si \ *■* •cj-, 8 ■ '-O -.2. 2J0 A .8 1.2 /.6 2.0 1.6 .4 .8 A2 Time,…
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