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NACA-TR-1224

Effects of wing position and fuselage size on the low-speed static rolling stability characteristics of a delta-wing model

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:23:06Z
date available2017-09-04T16:23:06Z
date copyright01/01/1955
date issued1955
identifier otherTRUYYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/86480
description abstractAn investigation was made to determine the effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of airplane models having a triangular wing and vertical tail surfaces. (author)
languageEnglish
titleNACA-TR-1224num
titleEffects of wing position and fuselage size on the low-speed static rolling stability characteristics of a delta-wing modelen
typestandard
page34
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1955
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAERODYNAMICS
subject keywordsAIRCRAFT
subject keywordsASSEMBLIES
subject keywordsBODY
subject keywordsCONFIGURATIONS
subject keywordsDELTA
subject keywordsDIMENSIONS
subject keywordsDYNAMICS
subject keywordsFLUID
subject keywordsFUSELAGES
subject keywordsINTERACTIONAL
subject keywordsLATERAL
subject keywordsLOCATION
subject keywordsLONGITUDINAL
subject keywordsLOW
subject keywordsMODELS
subject keywordsPOSITION
subject keywordsROLLING
subject keywordsSIZE
subject keywordsSPEED
subject keywordsSTABILITY
subject keywordsSTABILIZERS
subject keywordsSTATIC
subject keywordsTAIL
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS


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