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NACA-TR-766

Aerodynamic and hydrodynamic tests of a family of models of flying hulls derived from a streamline body - NACA model 84 series

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:36:28Z
date available2017-09-04T16:36:28Z
date copyright01/01/1943
date issued1943
identifier otherVCXUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/99992
description abstractA series of related forms of flying-boat hulls representing various degrees of compromise between aerodynamic and hydrodynamic requirements was tested in Langley Tank No. 1 and in the Langley 8-foot high-speed tunnel. The purpose of the investigation was to provide information regarding the penalties in water performance resulting from further aerodynamic refinement and, as a corollary, to provide information regarding the penalties in range or payload resulting from the retention of certain desirable hydrodynamic characteristics. The information should form a basis for over-all improvements in hull form.
languageEnglish
titleNACA-TR-766num
titleAerodynamic and hydrodynamic tests of a family of models of flying hulls derived from a streamline body - NACA model 84 seriesen
typestandard
page89
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1943
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAERODYNAMICS
subject keywordsAIRCRAFT
subject keywordsBALANCE
subject keywordsBODIES
subject keywordsBOWS
subject keywordsCONFIGURATIONS
subject keywordsDRAG
subject keywordsFOREBODIES
subject keywordsHULLS
subject keywordsHYDRODYNAMICS
subject keywordsLANDING
subject keywordsLIFT
subject keywordsMOMENTS
subject keywordsPITCHING
subject keywordsRESISTANCE
subject keywordsSTREAMLINED
subject keywordsSTRUCTURES
subject keywordsTAKEOFF
subject keywordsWATER


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