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NACA-TN-2504

Effects of wing position and horizontal-tail position on the static stability characteristics of models with unswept and 45 degree sweptback surfaces with some reference to mutual interference

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:23:34Z
date available2017-09-04T15:23:34Z
date copyright01/01/1951
date issued1951
identifier otherNFPTYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/23837
description abstractAn investigation was made to determine the effects of wing position and horizontal-tail position on the low-speed static longitudinal and static lateral stability characteristics of airplane models having unswept and 45° sweptback surfaces.
languageEnglish
titleNACA-TN-2504num
titleEffects of wing position and horizontal-tail position on the static stability characteristics of models with unswept and 45 degree sweptback surfaces with some reference to mutual interferenceen
typestandard
page59
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1951
contenttypefulltext
subject keywordsAIRPLANES
subject keywordsCOMBINATIONS
subject keywordsCOMPLETE
subject keywordsFUSELAGE
subject keywordsSTABILITY
subject keywordsSTATIC
subject keywordsSWEEP
subject keywordsTAIL
subject keywordsWING
subject keywordsWINGS


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