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NASA-CR-165843

Application of an aerodynamic analysis method including attainable thrust estimates to low speed leading-edge flap design for supersonic cruise vehicles

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:41:40Z
date available2017-09-04T17:41:40Z
date copyright01/01/1982
date issued1982
identifier otherDYMKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/164659
description abstractA study of low speed leading-edge flap design for supersonic cruise vehicle was conducted. Wings with flaps were analyzed with the aid of a newly developed subsonic wing program which provides estimates of attainable leading-edge thrust. Results indicate that the thrust actually attainable can have a significant influence on the design and that the resultant flaps can be smaller and simpler than those resulting from more conventional approaches.
languageEnglish
titleNASA-CR-165843num
titleApplication of an aerodynamic analysis method including attainable thrust estimates to low speed leading-edge flap design for supersonic cruise vehiclesen
typestandard
page29
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1982
contenttypefulltext
subject keywordsAIRCRAFT
subject keywordsANALYSIS
subject keywordsCOMPUTER
subject keywordsCRUISE
subject keywordsDESIGN
subject keywordsEDGE
subject keywordsESTIMATES
subject keywordsFLAPS
subject keywordsLEADING
subject keywordsPROGRAMS
subject keywordsRESEARCH
subject keywordsSUPERSONIC
subject keywordsTHRUST
subject keywordsWINGS


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