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NACA-TR-800

Effects of small angles of sweep and moderate amounts of dihedral on stalling and lateral characteristics of a wing-fuselage combination equipped with partial- and full-span double slotted flaps

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:23:04Z
date available2017-09-04T17:23:04Z
date copyright01/01/1944
date issued1944
identifier otherZXWUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/146266
description abstractTests of a wing-fuselage combinations incorporating NACA 65-series airfoil sections were conducted in the NACA 19-foot pressure tunnel. The investigation included the tests with flaps neutral and with partial- and full-span double slotted flaps deflected to determine the effects of (1) variations of wing sweep between -4 degrees and 8 degrees on stalling and lateral stability and control characteristics and (2) variations of dihedral between 0 degree and 6.75 degrees on lateral stability characteristics.
languageEnglish
titleNACA-TR-800num
titleEffects of small angles of sweep and moderate amounts of dihedral on stalling and lateral characteristics of a wing-fuselage combination equipped with partial- and full-span double slotted flapsen
typestandard
page20
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1944
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANGLE
subject keywordsBODY
subject keywordsCONFIGURATIONS
subject keywordsCONTROL
subject keywordsFLAPS
subject keywordsFORWARD
subject keywordsLATERAL
subject keywordsSLOTS
subject keywordsSTABILITY
subject keywordsSTALLING
subject keywordsSWEEP
subject keywordsSWEPT
subject keywordsSWEPTBACK
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS


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