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NACA-TR-400

The aerodynamic characteristics of a slotted Clark y wing as affected by the auxiliary airfoil position

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:58:06Z
date available2017-09-04T15:58:06Z
date copyright01/01/1932
date issued1932
identifier otherRBXUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/61283
description abstractAerodynamic force tests on a slotted Clark Y wing were conducted in a vertical wind tunnel to determine the best position for a given auxiliary airfoil with respect to the main wing. A systematic series of 100 changes in location of the auxiliary airfoil were made to cover all the probable useful ranges of slot gap, slot width, and slot depth. The results of the investigation may be applied to the design of automatic or controlled slots on wings with geometric characteristics similar to the wing tested. The best positions of the auxiliary airfoil were covered by the range of the tests, and the position for desired aerodynamic characteristics may easily be obtained from charts prepared especially for the purpose.
languageEnglish
titleNACA-TR-400num
titleThe aerodynamic characteristics of a slotted Clark y wing as affected by the auxiliary airfoil positionen
typestandard
page16
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1932
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRFOILS
subject keywordsANGLE
subject keywordsATTACK
subject keywordsCOEFFICIENTS
subject keywordsGEOMETRY
subject keywordsLIFT
subject keywordsLOCATION
subject keywordsPOSITION
subject keywordsPREVENTION
subject keywordsSLOTS
subject keywordsSTALLING
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS


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