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Two-dimensional wind-tunnel tests of a NASA supercritical airfoil with various high-lift systems Volume II - Test data

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:59:50Z
date available2017-09-04T15:59:50Z
date copyright01/01/1977
date issued1977
identifier otherRGNKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/62976
description abstractThree high lift systems for a 9.3 percent blunt based, supercritical airfoil were designed, fabricated, and wind tunnel tested. A method for calculating the viscous flow about two dimensional multicomponent airfoils was evaluated by comparing its predictions with test data. A comparison of high lift systems derived from supercritical airfoils with high lift systems derived from conventional airfoils is presented. The high lift systems for the supercritical airfoil were designed to achieve maximum lift and consisted of: (1) a single slotted flap, (2) a double slotted flap and a leading edge slat, and (3) a triple slotted flap and a leading edge slat. Aerodynamic force and moment data and surface pressure data are presented for all configurations and boundary layer and wake profiles for the single slotted flap configuration. The wind-tunnel models, test facilities and instrumentation, and data reduction are described.
languageEnglish
titleNASA-CR-2215num
titleTwo-dimensional wind-tunnel tests of a NASA supercritical airfoil with various high-lift systems Volume II - Test dataen
typestandard
page238
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1977
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRFOIL
subject keywordsCONTROL
subject keywordsFLAPS
subject keywordsFORCES
subject keywordsLIFT
subject keywordsMODELS
subject keywordsPROFILES
subject keywordsSUPERCRITICAL
subject keywordsSURFACES
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWINGS


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