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NASA-TN-D-4856

Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tail

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:06:50Z
date available2017-09-04T16:06:50Z
date copyright01/01/1968
date issued1968
identifier otherBHYKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/70057
description abstractAerodynamic characteristics of COIN aircraft model with boundary layer control on inverted V-tail
languageEnglish
titleNASA-TN-D-4856num
titleAerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted V-tailen
typestandard
page182
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1968
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsANGLE
subject keywordsASSEMBLIES
subject keywordsATTACK
subject keywordsBOUNDARY
subject keywordsCHARACTERISTICS
subject keywordsCOEFFICIENTS
subject keywordsCOIN
subject keywordsCONTROL
subject keywordsFLAPS
subject keywordsLAYER
subject keywordsLIFT
subject keywordsSLIPSTREAMS
subject keywordsSTABILITY
subject keywordsSURFACES
subject keywordsTAIL
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND


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