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NACA-TR-968

Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:45:58Z
date available2017-09-04T16:45:58Z
date copyright01/01/1950
date issued1950
identifier otherWAXUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/109212
description abstractA low-scale wind-tunnel investigation was conducted in rolling flow to determine the effects of aspect ratio and sweep (when varied independently) on the rolling stability derivatives for a series of untapered wings. The rolling-flow equipment of the Langley stability tunnel was used for the tests. The data of the investigation have been used to develop a method of accounting for the effects of the drag on the yawing moment due to rolling throughout the lift range.
languageEnglish
titleNACA-TR-968num
titleInvestigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wingsen
typestandard
page16
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1950
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsASPECT
subject keywordsCOEFFICIENTS
subject keywordsDAMPING
subject keywordsDERIVATIVES
subject keywordsDRAG
subject keywordsEFFECT
subject keywordsLATERAL
subject keywordsLIFT
subject keywordsLOW
subject keywordsMOMENTS
subject keywordsPARTS
subject keywordsRATIO
subject keywordsROLL
subject keywordsSPEED
subject keywordsSTABILITY
subject keywordsSUCTION
subject keywordsSWEEP
subject keywordsSWEPTBACK
subject keywordsTESTS
subject keywordsTIPS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS
subject keywordsYAWING


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