{"id":{"repo_id":"vt","oai_identifier":"oai:vtechworks.lib.vt.edu:10919/28591"},"canonical_url":"https://search.dev.ndltd.org/etd/vt/oai:vtechworks.lib.vt.edu:10919/28591","repository":{"repo_id":"vt","name":"Virginia Tech","base_url":"https://vtechworks.lib.vt.edu/oai/request"},"display":{"title":"Rotor/Fuselage Unsteady Interactional Aerodynamics: A New Computational Model","abstract":"A new unsteady rotor/fuselage interactional aerodynamics model has been developed. This model loosely couples a Generalized Dynamic Wake Theory (GDWT) to a Navier-Stokes solution procedure. This coupling is achieved using a newly developed unsteady pressure jump boundary condition in the Navier-Stokes model. The new unsteady pressure jump boundary condition models each rotor blade as a moving pressure jump which travels around the rotor azimuth =and is applied between two adjacent planes in a cylindrical, non-rotating grid. 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D."]},{"key":"dc:title","label":"Title","values":["Rotor/Fuselage Unsteady Interactional Aerodynamics: A New Computational Model"]}]}],"canonical_facts":{"dc:contributor.committeechair":["Barnwell, Richard W."],"dc:contributor.committeemember":["Jones, Henry","Devenport, William J.","Thomas, Russell H.","Mason, William H."],"dc:contributor.department":["Aerospace and Ocean Engineering"],"dc:creator":["Boyd, David Douglas Jr."],"dc:date.accessioned":["2014-03-14T20:14:59Z"],"dc:date.available":["2014-03-14T20:14:59Z","2000-08-13"],"dc:date.issued":["1999-07-27"],"dc:description.abstract":["A new unsteady rotor/fuselage interactional aerodynamics model has been developed. This model loosely couples a Generalized Dynamic Wake Theory (GDWT) to a Navier-Stokes solution procedure. This coupling is achieved using a newly developed unsteady pressure jump boundary condition in the Navier-Stokes model. 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