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NASA-TN-D-3437

Investigation of a semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control in hovering

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:50:25Z
date available2017-09-04T18:50:25Z
date copyright06/01/1966
date issued1966
identifier otherKUTKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/231874
description abstractHovering force-test on semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control
languageEnglish
titleNASA-TN-D-3437num
titleInvestigation of a semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control in hoveringen
typestandard
page76
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1966
contenttypefulltext
subject keywordsAERODYNAMICS
subject keywordsAIRCRAFT
subject keywordsEFFECT
subject keywordsFLAPPING
subject keywordsGROUND
subject keywordsHOVERING
subject keywordsMODEL
subject keywordsMODELS
subject keywordsSEMISPAN
subject keywordsTAKEOFF
subject keywordsTILT
subject keywordsVERTICAL
subject keywordsVTOL
subject keywordsWING
subject keywordsYAW


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