@inproceedings{Rwigema2010,
	title = {Propeller blade element momentum theory with vortex wake deflection},
	volume = {1},
	isbn = {978-1-61782-049-6},
	url = {http://www.icas.org/ICAS_ARCHIVE/ICAS2010/PAPERS/434.PDF},
	abstract = {Various propeller theories are treated in developing a model that analyses the aerodynamic performance of an aircraft propeller along with the construct and behaviour of the resultant slip-stream. Blade element momentum theory is used as a loworder aerodynamic model of the propeller and is coupled with a vortex wake representation of the slip-stream to relate the vorticity distributed throughout the slip-stream to the propeller forces. © 2010 by the International Council of Aeronautical Sciences - ICAS.},
	urldate = {2020-10-28},
	booktitle = {27th {Congress} of the {International} {Council} of the {Aeronautical} {Sciences}},
	author = {Rwigema, M. K.},
	year = {2010},
	keywords = {Blade element momentum, Propeller, Vortex wake, Wake deflection},
	pages = {727--735},
}

{"_id":"bX9akmLtn9T8AnxAF","bibbaseid":"rwigema-propellerbladeelementmomentumtheorywithvortexwakedeflection-2010","author_short":["Rwigema, M. K."],"bibdata":{"bibtype":"inproceedings","type":"inproceedings","title":"Propeller blade element momentum theory with vortex wake deflection","volume":"1","isbn":"978-1-61782-049-6","url":"http://www.icas.org/ICAS_ARCHIVE/ICAS2010/PAPERS/434.PDF","abstract":"Various propeller theories are treated in developing a model that analyses the aerodynamic performance of an aircraft propeller along with the construct and behaviour of the resultant slip-stream. Blade element momentum theory is used as a loworder aerodynamic model of the propeller and is coupled with a vortex wake representation of the slip-stream to relate the vorticity distributed throughout the slip-stream to the propeller forces. © 2010 by the International Council of Aeronautical Sciences - ICAS.","urldate":"2020-10-28","booktitle":"27th Congress of the International Council of the Aeronautical Sciences","author":[{"propositions":[],"lastnames":["Rwigema"],"firstnames":["M.","K."],"suffixes":[]}],"year":"2010","keywords":"Blade element momentum, Propeller, Vortex wake, Wake deflection","pages":"727–735","bibtex":"@inproceedings{Rwigema2010,\n\ttitle = {Propeller blade element momentum theory with vortex wake deflection},\n\tvolume = {1},\n\tisbn = {978-1-61782-049-6},\n\turl = {http://www.icas.org/ICAS_ARCHIVE/ICAS2010/PAPERS/434.PDF},\n\tabstract = {Various propeller theories are treated in developing a model that analyses the aerodynamic performance of an aircraft propeller along with the construct and behaviour of the resultant slip-stream. Blade element momentum theory is used as a loworder aerodynamic model of the propeller and is coupled with a vortex wake representation of the slip-stream to relate the vorticity distributed throughout the slip-stream to the propeller forces. © 2010 by the International Council of Aeronautical Sciences - ICAS.},\n\turldate = {2020-10-28},\n\tbooktitle = {27th {Congress} of the {International} {Council} of the {Aeronautical} {Sciences}},\n\tauthor = {Rwigema, M. K.},\n\tyear = {2010},\n\tkeywords = {Blade element momentum, Propeller, Vortex wake, Wake deflection},\n\tpages = {727--735},\n}\n\n\n\n","author_short":["Rwigema, M. K."],"key":"Rwigema2010","id":"Rwigema2010","bibbaseid":"rwigema-propellerbladeelementmomentumtheorywithvortexwakedeflection-2010","role":"author","urls":{"Paper":"http://www.icas.org/ICAS_ARCHIVE/ICAS2010/PAPERS/434.PDF"},"keyword":["Blade element momentum","Propeller","Vortex wake","Wake deflection"],"metadata":{"authorlinks":{}},"html":""},"bibtype":"inproceedings","biburl":"https://bibbase.org/zotero/dancili","dataSources":["sMzdddtr9jRe8zeKY"],"keywords":["blade element momentum","propeller","vortex wake","wake deflection"],"search_terms":["propeller","blade","element","momentum","theory","vortex","wake","deflection","rwigema"],"title":"Propeller blade element momentum theory with vortex wake deflection","year":2010}