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NACA-TR-1056

Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:56:11Z
date available2017-09-04T15:56:11Z
date copyright01/01/1951
date issued1951
identifier otherQXDZYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/59535
description abstractA simplified lifting-surface theory that includes effects of compressibility and spanwise variation of section lift-curve slope is used to provide charts with which antisymmetric loading due to arbitrary antisymmetric angle of attack can be found for wings having symmetric plan forms with a constant spanwise sweep angle of the quarter-chord line. Consideration is given to the flexible wing in roll. Aerodynamic characteristics due to rolling, deflected ailerons, and sideslip of wings with dihedral are considered. Solutions are presented for straight-tapered wings for a range of swept plan forms.
languageEnglish
titleNACA-TR-1056num
titleTheoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speedsen
typestandard
page40
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1951
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAILERONS
subject keywordsANTISYMMETRY
subject keywordsBODIES
subject keywordsCHARACTERISTICS
subject keywordsCOMPRESSIBILITY
subject keywordsCOMPUTATIONAL
subject keywordsDEFLECTION
subject keywordsDYNAMICS
subject keywordsEFFECTS
subject keywordsFLOW
subject keywordsFLUID
subject keywordsLOADING
subject keywordsLOADS
subject keywordsPLANFORMS
subject keywordsROLL
subject keywordsSIDESLIP
subject keywordsSPAN
subject keywordsSUBSONIC
subject keywordsSWEPT
subject keywordsSYMMETRICAL
subject keywordsWING
subject keywordsWINGS


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