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NACA-TN-2288

Estimation of low-speed lift and hinge-moment parameters for full-span trailing-edge flaps on lifting surfaces with and without sweepback

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1951

Abstract: Comparisons of the low-Speed experimental lift and hinge-moment parameters of flapped lifting surfaces with and without sweepback with values computed by several theoretical procedures are presented. Based on these limited results one theoretical method appears to be more s&- is factory than the other methods investigated and is therefore recommended for preliminary design estimates. to the section values of the lift and hinge-moment parameters for the effects of induced angle of attack and of induced camber to obtain the values for a finite aspect ratio. are obtained from the lift-Curve slopes calculated by the Weissinger method, and the induced-camber corrections are obtained from an adaptation of the Falkner lifting-surface procedure. recommended is based upon lifting-Surface theory, it may be applied without knowledge of this theory since the, necessary information is given in design charts presented herein and in NACA Rep. 921, 1948. Sample calculations are included.
URI: http://yse.yabesh.ir/std;jsessionid=47037D83FCDCAC426159DD6E273C9FCD/handle/yse/229467
Subject: AIRFOILS
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NACA-TN-2288

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:48:14Z
date available2017-09-04T18:48:14Z
date copyright01/01/1951
date issued1951
identifier otherKOEUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsessionid=47037D83FCDCAC426159DD6E273C9FCD/handle/yse/229467
description abstractComparisons of the low-Speed experimental lift and hinge-moment parameters of flapped lifting surfaces with and without sweepback with values computed by several theoretical procedures are presented. Based on these limited results one theoretical method appears to be more s&- is factory than the other methods investigated and is therefore recommended for preliminary design estimates. to the section values of the lift and hinge-moment parameters for the effects of induced angle of attack and of induced camber to obtain the values for a finite aspect ratio. are obtained from the lift-Curve slopes calculated by the Weissinger method, and the induced-camber corrections are obtained from an adaptation of the Falkner lifting-surface procedure. recommended is based upon lifting-Surface theory, it may be applied without knowledge of this theory since the, necessary information is given in design charts presented herein and in NACA Rep. 921, 1948. Sample calculations are included.
languageEnglish
titleNACA-TN-2288num
titleEstimation of low-speed lift and hinge-moment parameters for full-span trailing-edge flaps on lifting surfaces with and without sweepbacken
typestandard
page48
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1951
contenttypefulltext
subject keywordsAIRFOILS
subject keywordsBALANCED
subject keywordsCHARACTERISTICS
subject keywordsDISTRIBUTION
subject keywordsELEVATORS
subject keywordsFLAPS
subject keywordsGAP
subject keywordsHINGE
subject keywordsHORIZONTAL
subject keywordsLIFT
subject keywordsLIFTING
subject keywordsMOMENTS
subject keywordsNACA
subject keywordsSEALED
subject keywordsSPAN
subject keywordsSURFACE
subject keywordsSURFACES
subject keywordsSWEPTBACK
subject keywordsTAIL
subject keywordsTHEORIES
subject keywordsWING
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