Theoret. Comput. Fluid Dynamics: 213–237 Theoretical and Computational Fluid Dynamics © Springer-Verlag 1998 - Stokes boundary layer - Document - PDFSEARCH.IO

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	Theoret. Comput. Fluid Dynamics: 213–237 Theoretical and Computational Fluid Dynamics © Springer-Verlag 1998 Add to Reading List Document Date: 2010-09-08 02:56:25 Open Document File Size: 868,13 KB Share Result on Facebook City Oxford / / Company Rhodes Trust / Slm / IBM / EPSRC / Research Agreement / / Facility Princeton University / U.S.A. N.A. Pierce Oxford University Computing Laboratory / / IndustryTerm viscous solution / final converged design solution / optimum solution / flow solutions / flow solution / numerical solution / energy / gas constant / / Organization Princeton University / National Aeronautics and Space Administration / Department of Defense / Stokes Equations1 A. Jameson and L. Martinelli Department of Mechanical and Aerospace Engineering / U.S.A. N.A. Pierce Oxford University Computing Laboratory / / Person James Lighthill / / Position designer / / ProvinceOrState New Jersey / / Technology Fluid Dynamics / simulation / / SocialTag Calculus Aerodynamics Navier–Stokes equations Boundary layer Stokes flow Potential flow Inviscid flow Drag Euler equations Fluid dynamics

Theoret. Comput. Fluid Dynamics: 213–237 Theoretical and Computational Fluid Dynamics © Springer-Verlag 1998Add to Reading List