Abstract
This papers develops and implements a discrete adjoint formulation for a periodic, time-spectral discretization of the equations of fluid flow. Time-spectral flow solution methodologies have been proposed in order to significantly shorten the computational time for the solution of unsteady (periodic) flows with a narrow frequency spectrum. As such, these methodologies are only applicable to periodic flows encountered, for example, in turbomachinery, rotorcraft, and fixed-wing aeroelastic applications among other areas. For these classes of problems, the time-spectral discretization permits the solution of the corresponding adjoint equations and facilitates both design and error estimation / correction applications. Details of the discrete adjoint solver and its implementations are provided as well as its validation (through the calculation of sensitivities of unsteady flows) and some preliminary applications to mesh refinement / distribution in unsteady periodic flows. The procedure is found to be very robust and it is currently being extended to fundamental turbomachinery test cases.
Original language | English |
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Title of host publication | 44th AIAA Aerospace Sciences Meeting, Reno, Nevada, 9-12 January 2006 |
Subtitle of host publication | Collection of Technical Papers |
Publisher | American Institute of Aeronautics and Astronautics |
Pages | 8270-8285 |
Number of pages | 16 |
Volume | 11 |
ISBN (Electronic) | 978-1-62410-039-0 |
ISBN (Print) | 978-1-56347-807-9 |
DOIs | |
Publication status | Published - 1 Dec 2006 |
Externally published | Yes |
Event | 44th AIAA Aerospace Sciences Meeting 2006 - Reno, United States Duration: 9 Jan 2006 → 12 Jan 2006 Conference number: 44 |
Conference
Conference | 44th AIAA Aerospace Sciences Meeting 2006 |
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Country/Territory | United States |
City | Reno |
Period | 9/01/06 → 12/01/06 |