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dc.contributor.advisorWood, E. Roberts
dc.contributor.authorCuesta, Juan D.
dc.dateDecember 1994
dc.date.accessioned2014-08-13T20:26:31Z
dc.date.available2014-08-13T20:26:31Z
dc.date.issued1994-12
dc.identifier.urihttp://hdl.handle.net/10945/42794
dc.descriptionApproved for public release, distribution unlimiteden_US
dc.description.abstractRotor blade vibratory stresses are of utmost importance in helicopter design. A modified Myklestad-Prohl method for rotating beams has been coded to assist in preliminary helicopter rotor blade design. The rotor blade dynamics program is part of the Joint Army/Navy Rotorcraft Analysis and Design (JANRAD) program which was developed to aid in the preliminary design and analysis of helicopter rotor performance, stability and control, and rotor dynamics. JANRAD is an inter-active, user friendly program written in MATLAB* version 4.0 programming language and has been used extensively in the Naval Postgraduate School's capstone helicopter design course (AA 4306). A sample case is run and results are discussed.en_US
dc.format.extent66 p.en_US
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleModeling helicopter blade dynamics using a modified Myklestad-Prohl transfer matrix methoden_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.subject.authorNAen_US
dc.description.serviceU.S. Naval Reserve (USNR) authoren_US
dc.identifier.oclcocn640618544
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US


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