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NACA-RM-L8I08

Longitudinal-stability investigation of high-lift and stall-control devices on a 52 degree sweptback wing with and without fuselage and horizontal tail at a Reynolds number of 6.8 x 10(exp 6).

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:49:22Z
date available2017-09-04T17:49:22Z
date copyright01/01/1948
date issued1948
identifier otherETSWXDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/172588
description abstractContains low-speed longitudinal stability characteristics of a 52 degree sweptback wing of aspect ratio 2.88, taper ratio 0.625, and NACA 64 (sub 1)-112 airfoil sections normal to the 0.282-chord line, in combination with split flaps, leading-edge flaps, and upper-surface fences. Low-wing and midwing-fuselage aerodynamic characteristics are presented with and without a horizontal tail at various vertical locations. Tests were conducted at a Reynolds number of 6.8 x 10(exp 6).
languageEnglish
titleNACA-RM-L8I08num
titleLongitudinal-stability investigation of high-lift and stall-control devices on a 52 degree sweptback wing with and without fuselage and horizontal tail at a Reynolds number of 6.8 x 10(exp 6).en
typestandard
page43
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1948
contenttypefulltext
subject keywordsAIRPLANES
subject keywordsCOMBINATIONS
subject keywordsCOMPLETE
subject keywordsFLAPS
subject keywordsFUSELAGE
subject keywordsLONGITUDINAL
subject keywordsSTABILITY
subject keywordsSTATIC
subject keywordsSWEEP
subject keywordsTAIL
subject keywordsWING
subject keywordsWINGS


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