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NASA-TM-X-2313

Large-scale wind-tunnel tests of a propeller-driven deflected slipstream STOL model in ground effect

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:33:35Z
date available2017-09-04T18:33:35Z
date copyright01/01/1971
date issued1971
identifier otherJENKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/215827
description abstractWind tunnel tests of propellor driven, deflected slipstream, short takeoff aircraft model to determine longitudinal and lateral-directional stability when in ground effect
languageEnglish
titleNASA-TM-X-2313num
titleLarge-scale wind-tunnel tests of a propeller-driven deflected slipstream STOL model in ground effecten
typestandard
page46
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1971
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAERODYNAMICS
subject keywordsAIRCRAFT
subject keywordsCHARACTERISTICS
subject keywordsEFFECT
subject keywordsGROUND
subject keywordsMODELS
subject keywordsSHORT
subject keywordsSTABILITY
subject keywordsTAKEOFF
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND


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