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NACA-TN-2689

Effect of high-lift devices on the low-speed static lateral and yawing stability characteristics of an untapered 45 degrees sweptback wing

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:35:17Z
date available2017-09-04T18:35:17Z
date copyright01/01/1952
date issued1952
identifier otherJILUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=authoCA5893FD081D49A96159DD6EFDEC014A/handle/yse/217335
description abstractResults of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the static lateral stability derivatives and the yawing derivatives of an untapered 45 degrees sweptback wing are presented. The tests were made in the curved-flow test section of the Langley stability tunnel at a Reynolds number of 1.1 X 10 to the sixth power.
languageEnglish
titleNACA-TN-2689num
titleEffect of high-lift devices on the low-speed static lateral and yawing stability characteristics of an untapered 45 degrees sweptback wingen
typestandard
page21
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1952
contenttypefulltext
subject keywordsCOMPLETE
subject keywordsDAMPING
subject keywordsDERIVATIVES
subject keywordsDIRECTIONAL
subject keywordsEDGE
subject keywordsFLAPS
subject keywordsLATERAL
subject keywordsLEADING
subject keywordsSTABILITY
subject keywordsSTATIC
subject keywordsSWEEP
subject keywordsTRAILING
subject keywordsWINGS


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