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A flight investigation of short-period longitudinal oscillations of an airplane with free elevato

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:21:04Z
date available2017-09-04T18:21:04Z
date copyright01/01/1942
date issued1942
identifier otherHXUYYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/203531
description abstractA flight investigation has been made to check the results of a theoretical analysis of longitudinal stability of an airplane with free controls. Tests were made of a Fairchild XR2K-1 airplane on which the weight moment and the aerodynamic balance of the elevator were varied to bring it into a condition where unstable short-period oscillations were encountered. The amounts of aerodynamic balance and weight moment required for instability were found to be greater than the amounts predicted by the theory. Time histories of the oscillations are included to show the nature of the instability.
languageEnglish
titleNACA-WR-L-444num
titleA flight investigation of short-period longitudinal oscillations of an airplane with free elevatoen
typestandard
page22
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1942
contenttypefulltext


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