المؤلفون: Kivanç Ülker, Aee

المساهمون: The Pennsylvania State University CiteSeerX Archives

المصدر: http://etd.lib.metu.edu.tr/upload/12606976/index.pdf.

مصطلحات موضوعية: EULER/NAVIER-STOKES FLOW SOLVER

وصف الملف: application/pdf

Relation: http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.633.7368; http://etd.lib.metu.edu.tr/upload/12606976/index.pdf

الاتاحة: http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.633.7368
http://etd.lib.metu.edu.tr/upload/12606976/index.pdf

المؤلفون: Di Stefano, Martin, Hosder, Serhat, Baurle, Robert

المصدر: Mechanical and Aerospace Engineering Faculty Research & Creative Works

مصطلحات موضوعية: Chaos theory, Flow simulation, NASA, Navier Stokes equations, Polynomials, Ramjet engines, Reynolds equation, Sensitivity analysis, Turbulence models, Epistemic uncertainties, Model uncertainties, NASA Langley Research Center, Polynomial chaos theory, Relative sensitivity, Reynolds-averaged Navier Stokes flow solver, Uncertainty and sensitivity analysis, Uncertainty propagation, Uncertainty analysis, Aerospace Engineering

Relation: https://scholarsmine.mst.edu/mec_aereng_facwork/4238; https://doi.org/10.2514/6.2018-5262

الاتاحة: https://scholarsmine.mst.edu/mec_aereng_facwork/4238
https://doi.org/10.2514/6.2018-5262

المؤلفون: McGrory, William D.

المساهمون: AEROSOFT INC BLACKSBURG VA

المصدر: DTIC AND NTIS

مصطلحات موضوعية: Numerical Mathematics, Fluid Mechanics, COMPUTATIONAL FLUID DYNAMICS, NAVIER STOKES EQUATIONS, HYPERSONIC FLOW, COMPUTERIZED SIMULATION, GRIDS(COORDINATES), HYPERSONIC VEHICLES, UNSTRUCTURED NAVIER STOKES FLOW SOLVER

وصف الملف: text/html

Relation: http://www.dtic.mil/docs/citations/ADA399497

الاتاحة: http://www.dtic.mil/docs/citations/ADA399497
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA399497

المؤلفون: Von Stillfried, Florian, Lögdberg, Ola, Wallin, Stefan, Johansson, Arne V.

المصدر: 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. :2009

مصطلحات موضوعية: Computational grids, Computational results, Computational tools, Counter-rotating vortices, Defence research, Experimental data, Flat plate, Flow separation control, Governing equations, Grid generation, Highly sensitive, Local mesh refinement, Model approach, Navier-Stokes flow solver, Number of Grids, Physical effects, Pressure recovery, Royal Institute of Technology, Separation devices, Statistical effects, Statistical modeling, Stockholm, Time-consuming process, Turbulent boundary layers, Turbulent stress, Vortex generators, Vortex structures, Wall bounded flows, Aerospace engineering, Experiments, Flow separation, Mesh generation, Navier Stokes equations, Statistics, Three dimensional, Turbulent flow, Vortex flow, Computational fluid dynamics

وصف الملف: print

URL الوصول: https://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-152454

المؤلفون: AEROSOFT INC BLACKSBURG VA, McGrory, William D.

المصدر: DTIC AND NTIS

مصطلحات الفهرس: Numerical Mathematics, Fluid Mechanics, COMPUTATIONAL FLUID DYNAMICS, NAVIER STOKES EQUATIONS, HYPERSONIC FLOW, COMPUTERIZED SIMULATION, GRIDS(COORDINATES), HYPERSONIC VEHICLES., UNSTRUCTURED NAVIER STOKES FLOW SOLVER, Text

URL: https://apps.dtic.mil/docs/citations/ADA399497