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NACA-TR-1130

Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:31:14Z
date available2017-09-04T18:31:14Z
date copyright01/01/1953
date issued1953
identifier otherIYDZYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/213410
description abstractThe damping in yaw and the directional stability of a model freely oscillating in yaw were measured tail-off and tail-on and compared with the values obtained by theoretical consideration of the unsteady lift associated with an oscillating vertical tail. A range of low frequencies comparable to those of the lateral motions of airplanes was covered. The analysis includes the effects of vertical-tail aspect ratio and the two-dimensional effects of compressibility.
languageEnglish
titleNACA-TR-1130num
titleSome effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yawen
typestandard
page22
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1953
contenttypefulltext
subject keywordsAIRCRAFT
subject keywordsASPECT
subject keywordsASSEMBLIES
subject keywordsBODY
subject keywordsCOMPARISON
subject keywordsCOMPRESSIBILITY
subject keywordsCONFIGURATIONS
subject keywordsDAMPING
subject keywordsDERIVATIVES
subject keywordsDIRECTIONAL
subject keywordsDYNAMICS
subject keywordsEXPERIMENTATION
subject keywordsFLUID
subject keywordsFUSELAGES
subject keywordsLATERAL
subject keywordsMODELS
subject keywordsRATIO
subject keywordsSTABILITY
subject keywordsSTABILIZERS
subject keywordsSTATIC
subject keywordsTAIL
subject keywordsTESTS
subject keywordsTHEORIES
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS
subject keywordsYAW


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