Show simple item record

NASA-TN-D-4076

Static stability characteristics at Mach numbers from 1.90 to 4.63 of a 76 degrees swept arrow wing model with variations in horizontal-tail height, wing height, and dihedral

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:20:24Z
date available2017-09-04T15:20:24Z
date copyright01/01/1967
date issued1967
identifier otherASYKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/20301
description abstractHorizontal-tail height, wing height, and dihedral effects on longitudinal and lateral stability characteristics of 76 deg swept arrow wing aircraft model
languageEnglish
titleNASA-TN-D-4076num
titleStatic stability characteristics at Mach numbers from 1.90 to 4.63 of a 76 degrees swept arrow wing model with variations in horizontal-tail height, wing height, and dihedralen
typestandard
page119
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1967
contenttypefulltext
subject keywordsAIRCRAFT
subject keywordsANGLE
subject keywordsARROW
subject keywordsATTACK
subject keywordsDIHEDRAL
subject keywordsEFFECT
subject keywordsHORIZONTAL
subject keywordsLATERAL
subject keywordsLONGITUDINAL
subject keywordsMACH
subject keywordsMODEL
subject keywordsMODELS
subject keywordsNONLINEARITY
subject keywordsNUMBER
subject keywordsSIDESLIP
subject keywordsSTABILITY
subject keywordsSTATIC
subject keywordsSURFACES
subject keywordsSWEPT
subject keywordsTAIL
subject keywordsWING
subject keywordsWINGS


Files in this item

Thumbnail
Name:
ASYKAEAAAAAAAAAA.pdf
Size:
6.934Mb
Format:
PDF
View/Open

This item appears in the following Collection(s)

Show simple item record