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NACA-TR-572

Determination of the characteristics of tapered wings

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:11:00Z
date available2017-09-04T15:11:00Z
date copyright01/01/1937
date issued1937
identifier otherLSWUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/9352
description abstractThis report presents tables and charts for use in determining the characteristics of tapered wings. Theoretical factors are given from which the following characteristics of tapered wings may be found: the span lift distribution, the induced-angle-of attack distribution, the lift-curve slope, the angle of zero lift, the induced drag, the aerodynamic-center position, and the pitching moment about the aerodynamic center.
languageEnglish
titleNACA-TR-572num
titleDetermination of the characteristics of tapered wingsen
typestandard
page24
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1937
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsCENTER
subject keywordsCHARACTERISTICS
subject keywordsCHARTS
subject keywordsCOEFFICIENTS
subject keywordsCOMPUTATIONAL
subject keywordsDATA
subject keywordsDISTRIBUTION
subject keywordsDRAG
subject keywordsDYNAMICS
subject keywordsFLUID
subject keywordsFORCE
subject keywordsFORMULAS
subject keywordsLIFT
subject keywordsMOMENTS
subject keywordsPITCHING
subject keywordsPRESSURE
subject keywordsRATIO
subject keywordsSPAN
subject keywordsSWEPT
subject keywordsTABLES
subject keywordsTAILLESS
subject keywordsWING
subject keywordsWINGS


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