Show simple item record

NACA-WR-L-701

Test of NACA 66, 2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:32:21Z
date available2017-09-04T15:32:21Z
date copyright01/01/1942
date issued1942
identifier otherAXITDEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/33978
description abstractINTRODUCTION
At the request of the Army Air Forces, Materiel Command, tests have been made in the Langley two-dimensional low-turbulence pressure tunnel of a model of the NACA 66,2-116, a = 0,6 airfoil section representing the root section of the wing for the XP-63 airplane.
The data presented in this report consist of the following:
(a) Lift, drag, and flap hinge-moment characteristics for the internal, balanced flap.
(b) Lift, drag, and flap hinge-moment characteristics for the "modified" internal balanced flap.
(c) Lift and drag characteristics for the slotted flap.
The model was of 24-inch chord (cw), built of wood with dural slot cover plates for the flap. All flaps were equipped with pressure orifices.
languageEnglish
titleNACA-WR-L-701num
titleTest of NACA 66, 2-116, a = 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplaneen
typestandard
page20
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1942
contenttypefulltext
subject keywordsAIRFOILS
subject keywordsBALANCED
subject keywordsBELL
subject keywordsCHAR
subject keywordsDIM
subject keywordsDISTRIBUTION
subject keywordsDRAG
subject keywordsFLAPS
subject keywordsHINGE
subject keywordsLOW
subject keywordsMOMENTS
subject keywordsNACA
subject keywordsPRESSURE
subject keywordsSLOT
subject keywordsSLOTTED
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsTURBULENCE
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS


Files in this item

Thumbnail
Name:
AXITDEAAAAAAAAAA.pdf
Size:
984.3Kb
Format:
PDF
View/Open

This item appears in the following Collection(s)

Show simple item record