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dc.contributor.authorAhn, Jon
dc.date.accessioned2010-08-27T19:58:41Z
dc.date.available2010-08-27T19:58:41Z
dc.date.issued1997-02
dc.identifier.urihttp://hdl.handle.net/1721.1/57604
dc.description.abstractThe primary goal of this thesis is the application of the proven stream-surface based Newton method to analysis/design of an axisymmetric nacelle with the actuator disk modeling of a fan. And to further utilize the benefits of the Newton method, full attention is given to the linearized prediction of three-dimensional flow from a base axisymmetric solution, with an aim at replacing costly three-dimensional flow computations during initial nacelle design stages. The resulting code is to be called AMIS (Axisymmetric Multiple-passage Interacting Stream_surface Euler solver) to denote the lineage of Newton solver family pioneered by Drela and Giles, although AMIS has been built from scratch and share a few code lines.en_US
dc.language.isoen_USen_US
dc.publisherAerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, Massachusetts Institute of Technologyen_US
dc.relation.ispartofseriesACDL Technical Reports;FDRL TR-97-3
dc.titleAnalysis and design of axisymmetric transonic flow with linearized three-dimensional flow predictionen_US
dc.typeTechnical Reporten_US


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