dc.contributor.authorAtta, E. H.en_US
dc.contributor.authorYeung, Wai Hung.en_US
dc.date.accessioned2008-09-17T14:35:30Z
dc.date.available2008-09-17T14:35:30Z
dc.date.copyright1993en_US
dc.date.issued1993
dc.identifier.urihttp://hdl.handle.net/10356/6836
dc.description.abstractA computational method has been developed for the prediction of missile flow fields with emphasis on subsonic and transonic flight-conditions. The computational method is based on the thin shear layer formulation of the Navier-Stokes equations and a finite volume Runge-Kutta time marching algorithm.en_US
dc.rightsNanyang Technological Universityen_US
dc.subjectDRNTU::Engineering::Aeronautical engineering::Aerodynamics
dc.titleComputational methods of missile aerodynamicsen_US
dc.typeResearch Reporten_US
dc.contributor.schoolSchool of Mechanical & Production Engineeringen_US
dc.description.reportnumberARP-61-91


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