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NASA-TN-D-363

Investigation of the aerodynamic characteristics of a combination jet-flap and deflected-slipstream configuration at zero and low forward speeds

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1960

Abstract: An investigation of the aerodynamic characteristics of a semispan wing equipped with a 38.5-percent-chord sliding flap partially immersed in the slipstream of two propellers has been conducted in the 17-foot test section of the Langeley 300-MPH 7- by 10-foot tunnel. The wing had an aspect ratio of 7.0, taper ratio 1.0, and an NACA 63A412 airfoil section. The propellers were one wing chord in diameter. A jet of air was ejected over the knee of the flap through a momentum-coefficient range from zero to about 1.0.
URI: https://yse.yabesh.ir/std/handle/yse/28508
Subject: AERODYNAMIC
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    NASA-TN-D-363

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:27:34Z
date available2017-09-04T15:27:34Z
date copyright01/01/1960
date issued1960
identifier otherNRTKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/28508
description abstractAn investigation of the aerodynamic characteristics of a semispan wing equipped with a 38.5-percent-chord sliding flap partially immersed in the slipstream of two propellers has been conducted in the 17-foot test section of the Langeley 300-MPH 7- by 10-foot tunnel. The wing had an aspect ratio of 7.0, taper ratio 1.0, and an NACA 63A412 airfoil section. The propellers were one wing chord in diameter. A jet of air was ejected over the knee of the flap through a momentum-coefficient range from zero to about 1.0.
languageEnglish
titleNASA-TN-D-363num
titleInvestigation of the aerodynamic characteristics of a combination jet-flap and deflected-slipstream configuration at zero and low forward speedsen
typestandard
page73
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1960
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIR
subject keywordsCHARACTERISTICS
subject keywordsCOEFFICIENTS
subject keywordsCONTROL
subject keywordsDEFLECTION
subject keywordsDISTRIBUTION
subject keywordsFLAPS
subject keywordsFLOW
subject keywordsJET
subject keywordsPRESSURE
subject keywordsSURFACES
subject keywordsWING
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