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Aerodynamics / Tacoma Narrows Bridge / Vortex shedding / Turbulence modeling / Navier–Stokes equations / Computational fluid dynamics / Caisson / Reynolds number / Turbulence / Fluid dynamics / Fluid mechanics / Dynamics


Proceedings of FEDSM’03: 4TH ASME.JSME JOINT FLUIDS ENGINEERING CONFERENCE July 6-11, Honolulu, Hawaii FEDSM2003COMPUTATIONAL FLUID DYNAMICS MODEL FOR TACOMA
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Document Date: 2012-11-11 10:13:37

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File Size: 1,53 MB

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City

San Francisco / Tacoma / Columbus / Honolulu / Mountain View / /

Company

ANSYS Inc. / OEA Inc. / Farzin Shakib ACUSIM Software Inc. / Ocean Engineering Associates Inc. / Greyden Press / Bentley Inc. / Brigette Rosendall Bechtel National Inc. / Ames Aeronautical Laboratory / /

Country

United States / United Kingdom / /

Facility

pier Boundary Conditions Simulations / Stanford University / Tacoma Narrows Bridge / /

IndustryTerm

elements and nodes to different processors / finite element technology / approximate steady state solution / time integration algorithm / important tool / base algorithm / /

Movie

TACOMA NARROWS BRIDGE / /

Organization

National Advisory Committee for Aeronautics / United States Army / Stanford University / Department of Mechanical Engineering / /

Person

Noel K. Delany / Norman E. Sorenson / Jonathan Berkoe / /

Position

additional source model for projecting the inlet flow conditions / analyst / /

ProvinceOrState

California / Washington / /

SportsLeague

Stanford University / /

Technology

RAM / base algorithm / Galerkin/Least-Squares finite element technology / FLUID DYNAMICS / simulation / four 667 MHz Alpha processors / time integration algorithm / CAD / solved using the Galerkin/Least-Squares finite element technology / /

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