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Navier Stokes Simulation Of Quasi Axisymmetric And Three Dimensional Supersonic Vortex Breakdown
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Book Synopsis Navier-Stokes Simulation of Quasi-axisymmetric and Three-dimensional Supersonic Vortex Breakdown by : Hamdy A. Kandil
Download or read book Navier-Stokes Simulation of Quasi-axisymmetric and Three-dimensional Supersonic Vortex Breakdown written by Hamdy A. Kandil and published by . This book was released on 1993 with total page 454 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722792039 Total Pages :66 pages Book Rating :4.7/5 (92 download)
Book Synopsis Supersonic Quasi-Axisymmetric Vortex Breakdown by : National Aeronautics and Space Administration (NASA)
Download or read book Supersonic Quasi-Axisymmetric Vortex Breakdown written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-16 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: An extensive computational study of supersonic quasi-axisymmetric vortex breakdown in a configured circular duct is presented. The unsteady, compressible, full Navier-Stokes (NS) equations are used. The NS equations are solved for the quasi-axisymmetric flows using an implicit, upwind, flux difference splitting, finite volume scheme. The quasi-axisymmetric solutions are time accurate and are obtained by forcing the components of the flowfield vector to be equal on two axial planes, which are in close proximity of each other. The effect of Reynolds number, for laminar flows, on the evolution and persistence of vortex breakdown, is studied. Finally, the effect of swirl ration at the duct inlet is investigated. Kandil, Osama A. and Kandil, Hamdy A. and Liu, C. H. Langley Research Center...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722231293 Total Pages :82 pages Book Rating :4.2/5 (312 download)
Book Synopsis Analysis and Control of Supersonic Vortex Breakdown Flows by : National Aeronautics and Space Administration (NASA)
Download or read book Analysis and Control of Supersonic Vortex Breakdown Flows written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-06 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: Analysis and computation of steady, compressible, quasi-axisymmetric flow of an isolated, slender vortex are considered. The compressible, Navier-Stokes equations are reduced to a simpler set by using the slenderness and quasi-axisymmetry assumptions. The resulting set along with a compatibility equation are transformed from the diverging physical domain to a rectangular computational domain. Solving for a compatible set of initial profiles and specifying a compatible set of boundary conditions, the equations are solved using a type-differencing scheme. Vortex breakdown locations are detected by the failure of the scheme to converge. Computational examples include isolated vortex flows at different Mach numbers, external axial-pressure gradients and swirl ratios. Kandil, Osama A. Unspecified Center...
Book Synopsis Three-Dimensional Simulation of Vortex Breakdown by : National Aeronautics and Space Adm Nasa
Download or read book Three-Dimensional Simulation of Vortex Breakdown written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-11-12 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: The integral form of the complete, unsteady, compressible, three-dimensional Navier-Stokes equations in the conservation form, cast in generalized coordinate system, are solved, numerically, to simulate the vortex breakdown phenomenon. The inviscid fluxes are discretized using Roe's upwind-biased flux-difference splitting scheme and the viscous fluxes are discretized using central differencing. Time integration is performed using a backward Euler ADI (alternating direction implicit) scheme. A full approximation multigrid is used to accelerate the convergence to steady state. Kuruvila, G. and Salas, M. D. Langley Research Center...
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Book Synopsis Three-dimensional Supersonic Vortex Breakdown by : Osama A. Kandil
Download or read book Three-dimensional Supersonic Vortex Breakdown written by Osama A. Kandil and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Numerical Solutions to Three-dimensional Shock Wave by : Griffin Corpening
Download or read book Numerical Solutions to Three-dimensional Shock Wave written by Griffin Corpening and published by . This book was released on 1990 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Government Reports Annual Index written by and published by . This book was released on 1992 with total page 1388 pages. Available in PDF, EPUB and Kindle. Book excerpt: Sections 1-2. Keyword Index.--Section 3. Personal author index.--Section 4. Corporate author index.-- Section 5. Contract/grant number index, NTIS order/report number index 1-E.--Section 6. NTIS order/report number index F-Z.
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Book Synopsis Computational Fluid Dynamics by : John David Anderson
Download or read book Computational Fluid Dynamics written by John David Anderson and published by International Marine. This book was released on 1995-02 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt: A comprehensive, up to date text written for undergraduate and graduate students which covers topics ranging from the basic philosophy of computational fluid dynamics to advanced areas of CFD.
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