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NACA-TN-2010

Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:07:52Z
date available2017-09-04T17:07:52Z
date copyright01/01/1950
date issued1950
identifier otherYJAUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/131449
description abstractAn investigation has been conducted in the Langley stability tunnel to determine the effects of changes in horizontal-tail size and location on the static lateral stability characteristics of a complete model with wing and tail surfaces having the quarter-chord line swept back 45º.
Available procedures, based on analyses of unswept-tail configurations, for predicting the effect of the horizontal tail on directional stability, were found to be unreliable when applied to swept-tail configurations.
languageEnglish
titleNACA-TN-2010num
titleEffect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfacesen
typestandard
page47
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1950
contenttypefulltext
subject keywordsAIRFOILS
subject keywordsCHARACTERISTICS
subject keywordsCOMBINATIONS
subject keywordsDRAG
subject keywordsFUSELAGE
subject keywordsHORIZONTAL
subject keywordsLATERAL
subject keywordsLOW
subject keywordsNACA
subject keywordsORDINATES
subject keywordsPOSITION
subject keywordsSTABILITY
subject keywordsSTATIC
subject keywordsSURFACES
subject keywordsSWEPTBACK
subject keywordsTAIL
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS


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