An arbitrarily high-order, unstructured, free-wake panel solver
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2013.
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Thesis |
| Language: | eng |
| Published: |
Massachusetts Institute of Technology
2014
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/1721.1/85811 |
| _version_ | 1826193786786545664 |
|---|---|
| author | Moore, John Pease, IV |
| author2 | Jaime Peraire. |
| author_facet | Jaime Peraire. Moore, John Pease, IV |
| author_sort | Moore, John Pease, IV |
| collection | MIT |
| description | Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2013. |
| first_indexed | 2024-09-23T09:45:23Z |
| format | Thesis |
| id | mit-1721.1/85811 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T09:45:23Z |
| publishDate | 2014 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/858112019-04-10T09:03:21Z An arbitrarily high-order, unstructured, free-wake panel solver Moore, John Pease, IV Jaime Peraire. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2013. Cataloged from PDF version of thesis. Includes bibliographical references (pages 69-71). A high-order panel code capable of solving the potential flow equation about arbitrary curved geometries is presented. A new method for integrating curved, high-order panels using adaptive Gaussian quadrature is detailed. Furthermore, automated wake handling is addressed and a method to robustly solve for the steady-state free-wake rollup is proposed. Finally, a Fast Multipole Method with a complexity that scales as O(N) is also presented so that large problems can be handled using only a linear mesh. Results are presented to demonstrate high order accuracy and agreement with other inviscid solvers for a variety of test cases. by John Pease Moore IV. S.M. 2014-03-19T15:46:59Z 2014-03-19T15:46:59Z 2013 2013 Thesis http://hdl.handle.net/1721.1/85811 872121172 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 71 pages application/pdf Massachusetts Institute of Technology |
| spellingShingle | Aeronautics and Astronautics. Moore, John Pease, IV An arbitrarily high-order, unstructured, free-wake panel solver |
| title | An arbitrarily high-order, unstructured, free-wake panel solver |
| title_full | An arbitrarily high-order, unstructured, free-wake panel solver |
| title_fullStr | An arbitrarily high-order, unstructured, free-wake panel solver |
| title_full_unstemmed | An arbitrarily high-order, unstructured, free-wake panel solver |
| title_short | An arbitrarily high-order, unstructured, free-wake panel solver |
| title_sort | arbitrarily high order unstructured free wake panel solver |
| topic | Aeronautics and Astronautics. |
| url | http://hdl.handle.net/1721.1/85811 |
| work_keys_str_mv | AT moorejohnpeaseiv anarbitrarilyhighorderunstructuredfreewakepanelsolver AT moorejohnpeaseiv arbitrarilyhighorderunstructuredfreewakepanelsolver |