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NACA-TR-679

Wind-Tunnel Investigation of an N.A.C.A. 23012 Airfoil with a Slotted Flap and Three Types of Auxiliary Flap

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:05:29Z
date available2017-09-04T16:05:29Z
date copyright01/01/1939
date issued1939
identifier otherRVWUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/68654
description abstractA test installation was used in which an airfoil of 7-foot span was mounted vertically between the upper and the lower sides of the closed test section so that two-dimensional flow was approximated.
languageEnglish
titleNACA-TR-679num
titleWind-Tunnel Investigation of an N.A.C.A. 23012 Airfoil with a Slotted Flap and Three Types of Auxiliary Flapen
typestandard
page27
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1939
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRFOIL
subject keywordsAIRFOILS
subject keywordsCHARACTERISTICS
subject keywordsCOEFFICIENTS
subject keywordsDEVICES
subject keywordsDIMENSIONAL
subject keywordsDRAG
subject keywordsFLAPS
subject keywordsFLOW
subject keywordsLIFT
subject keywordsLOCATION
subject keywordsMOMENTS
subject keywordsPITCHING
subject keywordsPOSITION
subject keywordsPROFILES
subject keywordsSLOTS
subject keywordsSPLIT
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsTWO
subject keywordsWIND
subject keywordsWING


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