18th AIAA Computational Fluid Dynamics Conference
Latest Publications

TOTAL DOCUMENTS

133

(FIVE YEARS 0)

H-INDEX

(FIVE YEARS 0)

Published By American Institute Of Aeronautics And Astronautics

9781624101298

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Studies on Flow Transition Under Simulated Low Pressure Turbine Conditions Based on High-Order-LES Model

18th AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2007-3838 ◽

2007 ◽

Author(s):

Debasish Biswas

Keyword(s):

Low Pressure ◽

High Order ◽

Flow Transition ◽

Low Pressure Turbine ◽

Les Model

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Generation of Viscous Grid with Ridges and Corners

18th AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2007-3832 ◽

2007 ◽

Cited By ~ 2

Author(s):

Romain Aubry ◽

Rainald Lohner

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High-Order Central ENO Finite-Volume Scheme with Adaptive Mesh Refinement

18th AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2007-4323 ◽

2007 ◽

Cited By ~ 11

Author(s):

Lucian Ivan ◽

Clinton Groth

Keyword(s):

Finite Volume ◽

Adaptive Mesh Refinement ◽

Mesh Refinement ◽

Adaptive Mesh ◽

High Order ◽

Finite Volume Scheme ◽

Volume Scheme

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Numerical Evaluation and Optimization of Low Speed Wind Tunnel Contractions

18th AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2007-3827 ◽

2007 ◽

Cited By ~ 5

Author(s):

Con Doolan ◽

Rick Morgans

Keyword(s):

Wind Tunnel ◽

Numerical Evaluation ◽

Low Speed ◽

Low Speed Wind Tunnel

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Numerical Simulation of Homogeneous Equilibrium Two-Phase Flows with Shock-Stable Schemes

18th AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2007-4457 ◽

2007 ◽

Author(s):

Seung-Won Ihm ◽

Seok Woo Hong ◽

Sangho Han ◽

Chongam Kim

Keyword(s):

Numerical Simulation ◽

Two Phase Flows ◽

Two Phase ◽

Homogeneous Equilibrium

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Low-Diffusion Approximate Riemann Solvers for Reynolds-Stress Transport

18th AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2007-4467 ◽

2007 ◽

Cited By ~ 2

Author(s):

G. Gerolymos ◽

I. Vallet

Keyword(s):

Reynolds Stress ◽

Riemann Solvers ◽

Approximate Riemann Solvers

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Development of Stencil-Based Mesh Partitioning for Parallel Unstructured CFD Solvers

18th AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2007-4087 ◽

2007 ◽

Author(s):

Vladimyr Gidzak ◽

Ioannis Nompelis ◽

Graham Candler

Keyword(s):

Mesh Partitioning

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A Numerical Investigation of NACA0025 Airfoil Boundary Layer Using Large Eddy Simulations

18th AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2007-4199 ◽

2007 ◽

Cited By ~ 1

Author(s):

Tao Xu ◽

Pierre Sullivan ◽

Marius Paraschivoiu

Keyword(s):

Boundary Layer ◽

Numerical Investigation ◽

Large Eddy Simulations ◽

Large Eddy

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Numerical Investigations of Hypersonic Boundary Layer Transition over Circular Cones

18th AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2007-3843 ◽

2007 ◽

Cited By ~ 16

Author(s):

Frank Husmeier ◽

Hermann Fasel

Keyword(s):

Boundary Layer ◽

Boundary Layer Transition ◽

Hypersonic Boundary Layer ◽

Layer Transition ◽

Numerical Investigations

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Development of the Discrete Adjoint for a 3D Unstructured Euler Solver

18th AIAA Computational Fluid Dynamics Conference ◽

10.2514/6.2007-3954 ◽

2007 ◽

Author(s):

Giampietro Carpentieri ◽

Barry Koren ◽

Michel van Tooren

Keyword(s):

Discrete Adjoint ◽

Euler Solver

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18th AIAA Computational Fluid Dynamics ConferenceLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Studies on Flow Transition Under Simulated Low Pressure Turbine Conditions Based on High-Order-LES Model

Generation of Viscous Grid with Ridges and Corners

High-Order Central ENO Finite-Volume Scheme with Adaptive Mesh Refinement

Numerical Evaluation and Optimization of Low Speed Wind Tunnel Contractions

Numerical Simulation of Homogeneous Equilibrium Two-Phase Flows with Shock-Stable Schemes

Low-Diffusion Approximate Riemann Solvers for Reynolds-Stress Transport

Development of Stencil-Based Mesh Partitioning for Parallel Unstructured CFD Solvers

A Numerical Investigation of NACA0025 Airfoil Boundary Layer Using Large Eddy Simulations

Numerical Investigations of Hypersonic Boundary Layer Transition over Circular Cones

Development of the Discrete Adjoint for a 3D Unstructured Euler Solver

18th AIAA Computational Fluid Dynamics Conference
Latest Publications