Show simple item record

NASA-CR-2214

Two-dimensional wind-tunnel tests of a NASA supercritical airfoil with various high-lift systems. Volume 1: Data analysis

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:32:21Z
date available2017-09-04T15:32:21Z
date copyright01/01/1977
date issued1977
identifier otherOGNKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/33979
description abstractHigh-lift systems for a NASA, 9.3%, method for calculating the viscous flow about two-dimensional multicomponent airfoils was evaluated by comparing its predictions with test data. High-lift systems derived from supercritical airfoils were compared in terms of performance to high-lift systems derived from conventional airfoils. The high-lift systems for the supercritical airfoil were designed to achieve maximum lift and consisted of: a single-slotted flap; a double-slotted flap and a leading-edge slat; and a triple-slotted flap and a leading-edge slat. Agreement between theoretical predictions and experimental results are also discussed.
languageEnglish
titleNASA-CR-2214num
titleTwo-dimensional wind-tunnel tests of a NASA supercritical airfoil with various high-lift systems. Volume 1: Data analysisen
typestandard
page91
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1977
contenttypefulltext
subject keywordsAIRFOILS
subject keywordsBOUNDARY
subject keywordsCONTROL
subject keywordsDIMENSIONAL
subject keywordsEDGE
subject keywordsLAYER
subject keywordsLEADING
subject keywordsLIFT
subject keywordsSLATS
subject keywordsSUPERCRITICAL
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsTWO
subject keywordsWAKES
subject keywordsWIND
subject keywordsWINGS


Files in this item

Thumbnail
Name:
OGNKAEAAAAAAAAAA.pdf
Size:
1.856Mb
Format:
PDF
View/Open

This item appears in the following Collection(s)

Show simple item record