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NACA-WR-L-662

Tests of two models representing intermediate inboard and outboard wing sections of the XB-36 airplane

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:35:59Z
date available2017-09-04T18:35:59Z
date copyright01/01/1943
date issued1943
identifier otherJKAZYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/217952
description abstractINTRODUCTION
At the request of the Army air Forces, Material Command, tests were made in the two-dimensional low-turbulence pressure tunnel and the two-dimensional low-turbulence tunnel of two models submitted by the Consolidated Aircraft Corporation.
The model representing the inboard section was tested with four combinations of flap shape and slot entry to obtain the best slotted flap characteristics on the basis of maximum section lift coefficient and minimum section drag coefficient when retracted. The combination chosen was then tested to determine the effect of varying the gap with flap in the maximum lift position. Tests on this section included lift, drag, pressure-distribution measurements, and pitching moments for various flap deflections δf. A scale-effect test was made on the section with flap retracted and at maximum lift position.
languageEnglish
titleNACA-WR-L-662num
titleTests of two models representing intermediate inboard and outboard wing sections of the XB-36 airplaneen
typestandard
page36
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1943
contenttypefulltext
subject keywordsAILERONS
subject keywordsAIRFOILS
subject keywordsBALANCED
subject keywordsCHAR
subject keywordsCONSOLIDATED
subject keywordsDEFLECTION
subject keywordsDIM
subject keywordsDRAG
subject keywordsFLAPS
subject keywordsLOW
subject keywordsMOMENTS
subject keywordsNACA
subject keywordsPRESS
subject keywordsPRESSURE
subject keywordsSLOTTED
subject keywordsSPLIT
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsTURBULENCE
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS


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