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Propellers in yaw

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:31:26Z
date available2017-09-04T18:31:26Z
date copyright01/01/1945
date issued1945
identifier otherIYWUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/213683
description abstractIt was realized as early as 1909 that a propeller in yaw develops a side force like that of a fin. In 1917, R. G. Harris expressed this force in terms of the torque coefficient for the unyawed propeller. Of several attempts to express the side force directly in terms of the shape of the blades, however, none has been completely satisfactory. An analysis that incorporates induction effects not adequately covered in previous work and that gives good agreement with experiment over a wide range of operating conditions is presented. The present analysis shows that the fin analogy may be extended to the form of the side-force expression and that the effective fin area may be taken as the projected side area of the propeller.
languageEnglish
titleNACA-TR-820num
titlePropellers in yawen
typestandard
page23
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1945
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsASPECT
subject keywordsCOMPRESSIBILITY
subject keywordsCONTRAROTATING
subject keywordsEFFECTS
subject keywordsFORCES
subject keywordsINCLINATION
subject keywordsMOMENTS
subject keywordsPITCH
subject keywordsPROPELLERS
subject keywordsRATIO
subject keywordsSTABILITY
subject keywordsYAW


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