Abstract
An Euler solution algorithm is presented for the computation of unsteady flows about manoeuvring aircraft. The algorithm employs an implicit multi-grid time march, coupled with an unstructured patched-interface procedure, to increase both efficiency and flexibility when applied to realistic configurations. Example Indicial-plunge functions are computed for a representative aircraft wing-tail geometry, using both patched and continuous meshes. The results illustrate the ability of the algorithm to capture vortex-flow interaction phenomena relevant to aircraft dynamic response.
Original language | English |
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Title of host publication | 14th Applied Aerodynamics Conference 1996 |
Subtitle of host publication | 17 June 1996 - 20 June 1996, New Orleans, LA, U.S.A. |
Place of Publication | Reston, VA |
Publisher | Aerospace Research Central |
Pages | 852-858 |
Number of pages | 7 |
ISBN (Print) | 9781563472121 |
DOIs | |
Publication status | Published - 1 Jan 1996 |
Externally published | Yes |
Event | 14th Applied Aerodynamics Conference 1996 - New Orleans, United States Duration: 17 Jun 1996 → 20 Jun 1996 Conference number: 14 |
Publication series
Name | AIAA Meeting Paper |
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Publisher | Aerospace Research Central |
Number | 96-2485 |
ISSN (Print) | 0146-3705 |
Conference
Conference | 14th Applied Aerodynamics Conference 1996 |
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Country/Territory | United States |
City | New Orleans |
Period | 17/06/96 → 20/06/96 |