dc.contributor.author | Ahn, Jon | |
dc.date.accessioned | 2010-08-27T19:58:41Z | |
dc.date.available | 2010-08-27T19:58:41Z | |
dc.date.issued | 1997-02 | |
dc.identifier.uri | http://hdl.handle.net/1721.1/57604 | |
dc.description.abstract | The 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.iso | en_US | en_US |
dc.publisher | Aerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, Massachusetts Institute of Technology | en_US |
dc.relation.ispartofseries | ACDL Technical Reports;FDRL TR-97-3 | |
dc.title | Analysis and design of axisymmetric transonic flow with linearized three-dimensional flow prediction | en_US |
dc.type | Technical Report | en_US |