The effect of lateral controls in producing motion of an airplane as computed from wind-tunnel dataAn analytical study of the lateral controllability of an airplane has been made in which both the static rolling and yawing moments supplied by the controls and the reactions due to the inherent stability of the airplane have been taken into account. A hypothetical average airplane, embodying the essential characteristics of both the wind tunnel models and the full size test airplanes, was assumed for the study. Computations made of forced rolling and yawing motions of an F-22 airplane caused by a sudden deflection of the ailerons were found to agree well with actual measurements of these motions. The conditions following instantaneous full deflections of the lateral control have been studied, and some attention has been devoted to the controlling of complete turn maneuvers.
Document ID
19760011975
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Weick, F. E. (NASA Langley Research Center Hampton, VA, United States)
Jones, R. T. (NASA Langley Research Center Hampton, VA, United States)