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The rolling moment due to sideslip of swept wings at subsonic and transonic speeds

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:42:04Z
date available2017-09-04T16:42:04Z
date copyright01/01/1960
date issued1960
identifier otherVQTKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/105374
description abstractAn analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.
In view of the need for reliable procedures for estimating rolling moment due to sideslip at high subsonic speeds, new methods have been derived and design charts are presented for estimating the effects of compressibility and wing geometry. The overall agreement between estimated and experimental results indicated that the effects of win g aspect ratio, taper ratio, sweep, and dihedral on the rolling moment due to side-slip of wing-fuselage configurations for sideslip angles up to ±5° could be estimated with reasonable accuracy up to the force-break Mach number at low lift coefficients.
languageEnglish
titleNASA-TN-D-209num
titleThe rolling moment due to sideslip of swept wings at subsonic and transonic speedsen
typestandard
page82
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1960
contenttypefulltext
subject keywordsASPECT
subject keywordsBODY
subject keywordsCOMPRESSIBILITY
subject keywordsCONFIGURATIONS
subject keywordsGEOMETRY
subject keywordsMACH
subject keywordsMOMENTS
subject keywordsNUMBER
subject keywordsRATIO
subject keywordsROLLING
subject keywordsSIDESLIP
subject keywordsSPEED
subject keywordsSUBSONIC
subject keywordsSWEPT
subject keywordsTESTS
subject keywordsTRANSONIC
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS


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