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Investigation of full-scale split trailing-edge wing flaps with various chords and hinge locations

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:27:37Z
date available2017-09-04T15:27:37Z
date copyright01/01/1936
date issued1936
identifier otherNRWUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/28566
description abstractThis report gives the results of an investigation conducted in the NACA full-scale wind tunnel on a small parasol monoplane equipped with three different split trailing-edge wing flaps. The object of the investigation was to determine and correlate data on the characteristics of the airplane and flaps as affected by variation in flap chord, flap deflection, and flap location along the wing chord. The results give the lift, the drag, and the pitching moment characteristics of the airplane, and the flap forces and moments, the pressure distribution over the flaps and wing at one section, and the downwash characteristics of the flap and wing combinations.
languageEnglish
titleNACA-TR-539num
titleInvestigation of full-scale split trailing-edge wing flaps with various chords and hinge locationsen
typestandard
page26
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1936
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsDISTRIBUTION
subject keywordsDRAG
subject keywordsEDGE
subject keywordsFLAPS
subject keywordsFORCES
subject keywordsFULL
subject keywordsHINGES
subject keywordsLIFT
subject keywordsLOCATION
subject keywordsMOMENTS
subject keywordsMONOPLANES
subject keywordsPITCHING
subject keywordsPOSITION
subject keywordsPRESSURE
subject keywordsSCALE
subject keywordsSPLIT
subject keywordsTESTS
subject keywordsTRAILING
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING


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