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NASA-TT-F-823

Theory of the lifting airscrew

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:21:57Z
date available2017-09-04T16:21:57Z
date copyright01/01/1976
date issued1976
identifier otherTOWWAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/85366
description abstractThe vortex theory, and some aspects of velocity potential were discussed. Oblique and axial translations of a lifting airscrew in an ideal fluid are considered first, within the limits of linear and nonlinear theories. Then, viscosity and compressibility effects are introduced. Exposition of some aspects of propeller operation in a compressible medium concludes this presentation.
languageEnglish
titleNASA-TT-F-823num
titleTheory of the lifting airscrewen
typestandard
page481
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1976
contenttypefulltext
subject keywordsAERODYNAMICS
subject keywordsCOMPRESSIBLE
subject keywordsDISTRIBUTION
subject keywordsFLOW
subject keywordsFLUIDS
subject keywordsIDEAL
subject keywordsLIFTING
subject keywordsPOTENTIAL
subject keywordsPROPELLERS
subject keywordsROTOR
subject keywordsROTORS
subject keywordsTHEORY
subject keywordsVELOCITY
subject keywordsVISCOUS
subject keywordsVORTICES


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