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NASA-TP-1889

Wing-alone aerodynamic characteristics for high angles of attack of supersonic speeds

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:35:32Z
date available2017-09-04T15:35:32Z
date copyright01/01/1981
date issued1981
identifier otherOPWWAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/37465
description abstractAn experiment was conducted to determine wing-alone supersonic aerodynamic characteristics at high angles of attack. The wings tested varied in aspect ratio from 0.5 to 4.0 and in taper ratio from 0 to 1.0. The wings were tested at angles of attack ranging rom -5 deg to 60 deg and at Mach number from 1.60 to 4.60. The aerodynamic characteristics were obtained by integrating local pressures measured over the wing surfaces. Presented and discussed are results showing the effects of aspect ratio, taper ratio, Mach number, and angle of attack on force and moment coefficients and center of pressure locations. Also included are tabulations of the pressure measurements.
languageEnglish
titleNASA-TP-1889num
titleWing-alone aerodynamic characteristics for high angles of attack of supersonic speedsen
typestandard
page191
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1981
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANGLE
subject keywordsASPECT
subject keywordsATTACK
subject keywordsCHARACTERISTICS
subject keywordsDATA
subject keywordsDISTRIBUTION
subject keywordsMACH
subject keywordsNUMBER
subject keywordsPRESSURE
subject keywordsRATIO
subject keywordsSPEED
subject keywordsSUPERSONIC
subject keywordsTABLES
subject keywordsWINGS


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