Show simple item record

dc.contributor.advisorSchmidt, Louis V.
dc.contributor.authorLancaster, Emmet John
dc.dateJune 1977
dc.date.accessioned2012-11-16T19:15:31Z
dc.date.available2012-11-16T19:15:31Z
dc.date.issued1977-06
dc.identifier.urihttp://hdl.handle.net/10945/18154
dc.descriptionApproved for public release; distribution is unlimited
dc.description.abstractSteady state results of lift developed by varying the momentum blowing coefficient (C(ϻ)) upon a refurbished Circulation Control Rotor (CCR) airfoil section were favorable. This thesis was an experimental investigation to quantitatively evaluate whether the steady state results could be applied by a quasi-steady assumption when a harmonic perturbation of C(ϻ) was superimposed upon the steady value. Results suggested an attenuation in the dynamic transfer function of dC(p)/dC(ϻ) as the oscillating blowing frequency was increased.
dc.description.urihttp://archive.org/details/initialunsteadya00lanc
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.
dc.subject.lcshAeronauticsen_US
dc.titleInitial unsteady aerodynamic measurements of a circulation controlled airfoil and an oscillating flow wind tunnel.en_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentAeronautics
dc.description.serviceLieutenant, United States Navy
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record