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Subsonic aerodynamic characteristics of interacting lifting surfaces with separated flow around sharp edges predicted by a vortex-lattice method

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:55:02Z
date available2017-09-04T15:55:02Z
date copyright01/01/1975
date issued1975
identifier otherQTYKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/58380
description abstractBecause the potential flow suction along the leading and side edges of a planform can be used to determine both leading- and side-edge vortex lift, the present investigation was undertaken to apply the vortex-lattice method to computing side-edge suction force for isolated or interacting planforms. Although there is a small effect of bound vortex sweep on the computation of the side-edge suction force, the results obtained for a number of different isolated planforms produced acceptable agreement with results obtained from a method employing continuous induced-velocity distributions. By using the method outlined, better agreement between theory and experiment was noted for a wing in the presence of a canard than was previously obtained.
languageEnglish
titleNASA-TN-D-7921num
titleSubsonic aerodynamic characteristics of interacting lifting surfaces with separated flow around sharp edges predicted by a vortex-lattice methoden
typestandard
page94
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1975
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsBODIES
subject keywordsCHARACTERISTICS
subject keywordsEDGES
subject keywordsFLOW
subject keywordsLATTICE
subject keywordsLATTICES
subject keywordsLEADING
subject keywordsLIFTING
subject keywordsMATHEMATICS
subject keywordsMETHOD
subject keywordsPLANFORMS
subject keywordsSEPARATED
subject keywordsSHARP
subject keywordsSUBSONIC
subject keywordsSUCTION
subject keywordsVORTEX
subject keywordsVORTICES


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