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NACA-TR-819

Formulas for propellers in yaw and charts of the side-force derivative

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:01:15Z
date available2017-09-04T18:01:15Z
date copyright01/01/1945
date issued1945
identifier otherFYWUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/184345
description abstractGeneral formulas are given for propellers for the rate of change of side-force coefficient with angle of yaw and for the rate of change of pitching-moment coefficient with angle of yaw. Charts of the side-force derivative are given for two propellers of different plan form. The charts cover solidities of two to six blades and single and dual rotation. The blade angle ranges from 15 degrees or 20 degrees to 60 degrees.
languageEnglish
titleNACA-TR-819num
titleFormulas for propellers in yaw and charts of the side-force derivativeen
typestandard
page18
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1945
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANGLES
subject keywordsASPECT
subject keywordsBLADES
subject keywordsCOMPUTATION
subject keywordsCONTRAROTATING
subject keywordsDOWNWASH
subject keywordsFORCES
subject keywordsFORMULAS
subject keywordsGEOMETRY
subject keywordsMATHEMATICS
subject keywordsMOMENTS
subject keywordsPITCHING
subject keywordsPROPELLER
subject keywordsPROPELLERS
subject keywordsRATIO
subject keywordsUPWASH
subject keywordsWINGS
subject keywordsYAW


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