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FastAero – A Precorrected FFT – Fast Multipole Tree Steady and Unsteady Potential Flow Solver

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dc.contributor.author Willis, David
dc.contributor.author Peraire, Jaime
dc.contributor.author White, Jacob K.
dc.date.accessioned 2004-12-10T16:57:29Z
dc.date.available 2004-12-10T16:57:29Z
dc.date.issued 2005-01
dc.identifier.uri http://hdl.handle.net/1721.1/7378
dc.description.abstract In this paper a precorrected FFT-Fast Multipole Tree (pFFT-FMT) method for solving the potential flow around arbitrary three dimensional bodies is presented. The method takes advantage of the efficiency of the pFFT and FMT algorithms to facilitate more demanding computations such as automatic wake generation and hands-off steady and unsteady aerodynamic simulations. The velocity potential on the body surfaces and in the domain is determined using a pFFT Boundary Element Method (BEM) approach based on the Green’s Theorem Boundary Integral Equation. The vorticity trailing all lifting surfaces in the domain is represented using a Fast Multipole Tree, time advected, vortex participle method. Some simple steady state flow solutions are performed to demonstrate the basic capabilities of the solver. Although this paper focuses primarily on steady state solutions, it should be noted that this approach is designed to be a robust and efficient unsteady potential flow simulation tool, useful for rapid computational prototyping. en
dc.description.sponsorship Singapore-MIT Alliance (SMA) en
dc.format.extent 5161518 bytes
dc.format.mimetype application/pdf
dc.language.iso en
dc.relation.ispartofseries High Performance Computation for Engineered Systems (HPCES);
dc.subject Aerodynamics en
dc.subject Panel Method en
dc.subject Boundary Element Method en
dc.subject precorrected FFT en
dc.title FastAero – A Precorrected FFT – Fast Multipole Tree Steady and Unsteady Potential Flow Solver en
dc.type Article en


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