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Lateral control required for satisfactory flying qualities based on flight tests of numerous airplanes

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:15:23Z
date available2017-09-04T16:15:23Z
date copyright01/01/1941
date issued1941
identifier otherSWWUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/78641
description abstractReport presents the results of an analysis made of the aileron control characteristics of numerous airplanes tested in flight by the National Advisory Committee for Aeronautics. By the use of previously developed theory, the observed values of pb/2v for the various wing-aileron arrangements were examined to determine the effective section characteristics of the various aileron types.
languageEnglish
titleNACA-TR-715num
titleLateral control required for satisfactory flying qualities based on flight tests of numerous airplanesen
typestandard
page7
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1941
contenttypefulltext


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