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dc.contributor.advisorSchmidt, Louis V.
dc.contributor.authorCline, John Hendrix
dc.dateMarch 1977
dc.date.accessioned2012-11-16T19:16:50Z
dc.date.available2012-11-16T19:16:50Z
dc.date.issued1977-03
dc.identifier.urihttp://hdl.handle.net/10945/18286
dc.descriptionApproved for public release; distribution is unlimiteden_US
dc.description.abstractThe rotor system of the proposed XH-2/CCR (Circulation Control Rotor) prototype aircraft and the state variable format of the airframe equations of motion are described. Through a study of the eigenvalues and eigenvectors of the basic airframe. the effect of uncoupling and cross-coupling the helicopter equation of motions were analyzed. The control matrix for the CCR was then generated using an applicable pneumatic lead angle for Coanda blowing. Feedback gains, to give the aircraft acceptable flying qualities, were calculated for the Stability Augmentation System (SAS) and finally the aircraft's sensitivity to changes in pneumatic lead angles were studied. the programs used in the above study (capable of handling up to 10 X 10 matrices) are listed for both the IBM-360 and HP-9830 mini-computer.en_US
dc.description.urihttp://archive.org/details/stabilityanalysi00clin
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. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted.en_US
dc.subject.lcshAeronauticsen_US
dc.titleA stability analysis of the proposed circulation control rotor (CCR) prototypeen_US
dc.typeThesisen_US
dc.contributor.secondreaderLayton, Donald M.
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentDepartment of Aeronautics
dc.subject.authorCirculation control rotor (CCR)en_US
dc.subject.authorHX-2/CCRen_US
dc.subject.authorBASMATen_US
dc.description.serviceLieutenant, United States Navyen_US
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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