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NASA-TN-D-4929

Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:45:47Z
date available2017-09-04T18:45:47Z
date copyright01/01/1968
date issued1968
identifier otherKHYKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=authoCA5893FD081D49A96159DD6EFDEC014A/handle/yse/227120
description abstractComputing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in compressible flow
languageEnglish
titleNASA-TN-D-4929num
titleTheory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flowen
typestandard
page79
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1968
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANGLE
subject keywordsATTACK
subject keywordsCOMPRESSIBILITY
subject keywordsCOMPRESSIBLE
subject keywordsEFFECTS
subject keywordsFLOW
subject keywordsLOADING
subject keywordsROLL
subject keywordsSIDESLIP
subject keywordsSPAN
subject keywordsSTABILITY
subject keywordsVORTICES
subject keywordsWING
subject keywordsYAW


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