Show simple item record

NACA-TN-D-8361

Effects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:52:42Z
date available2017-09-04T16:52:42Z
date copyright01/01/1976
date issued1976
identifier otherWTYKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/116267
description abstractAn investigation was conducted in the Langley low turbulence pressure tunnel to determine the effects of wing leading edge radius and Reynolds number on the longitudinal aerodynamic characteristics of a series of highly swept wing-body configurations. The tests were conducted at Mach numbers below 0.30, angles of attack up to 16 deg, and Reynolds numbers per meter from 6.57 million to 43.27 million. The wings under study in this investigation had leading edge sweep angles of 61.7 deg, 64.61 deg, and 67.01 deg in combination with trailing edge sweep angles of 0 deg and 40.6 deg. The leading edge radii of each wing planform could be varied from sharp to nearly round.
languageEnglish
titleNACA-TN-D-8361num
titleEffects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speedsen
typestandard
page56
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1976
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsANGLE
subject keywordsATTACK
subject keywordsCHARACTERISTICS
subject keywordsDESIGN
subject keywordsEDGE
subject keywordsLEADING
subject keywordsLONGITUDINAL
subject keywordsMACH
subject keywordsNUMBER
subject keywordsPLANFORMS
subject keywordsPROFILES
subject keywordsREYNOLDS
subject keywordsSTABILITY
subject keywordsSUPERSONIC
subject keywordsSWEEP
subject keywordsSWEPT
subject keywordsWING
subject keywordsWINGS


Files in this item

Thumbnail
Name:
WTYKAEAAAAAAAAAA.pdf
Size:
2.791Mb
Format:
PDF
View/Open

This item appears in the following Collection(s)

Show simple item record