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Showing 1 to 20 of 116 for “"Reynolds Averaged Navier-Stokes (RANS)"”.

  1. Geometry-Aware Modeling of Rough-Wall Turbulence Using Reynolds-Averaged Navier-Stokes (RANS) Frameworks

    … role in drag prediction, energy efficiency, and transport processes in internal and external flows. Despite extensive research, the representation of roughness effects in Reynolds-Averaged NavierStokes (RANS) turbulence models remains fundamentally challenging. Classical approaches rely on …

    sask Repository record for Geometry-Aware Modeling of Rough-Wall Turbulence Using Reynolds-Averaged Navier-Stokes (RANS) Frameworks (opens in a new tab)

  2. Quantification of structural uncertainties in RANS turbulence models

    … model for the structural uncertainties in Reynolds averaged Navier-Stokes (RANS) turbulence models. This approach solves an inference problem by comparing the results of RANS calculations to direct numerical simulation. The adjoint method is used to efficiently solve an inverse problem to …

    mit Repository record for Quantification of structural uncertainties in RANS turbulence models (opens in a new tab)

  3. Experimental and Numerical Study of Air Flows in a Full Scale Room

    Different turbulence models based on the Reynolds-Averaged Navier-Stokes (RANS) method and the Large Eddy Simulation (LES) with dynamical subgrid model were evaluated with the experimental data from the VPSTV measurements. The LES provided the best predictions for the three ventilation rates while …

    uiuc Repository record for Experimental and Numerical Study of Air Flows in a Full Scale Room (opens in a new tab)

  4. Design and Numerical Evaluation of a Counter- Rotating Compressor in the Absence of Boundary Layer Control: Part II

    … two-dimensional, and three dimensional Reynolds averaged Navier-Stokes (RANS) analyses were conducted to verify the design. Additionally, splitter blades were introduced in the first stage rotor as a means of providing mechanical flow control. The two-dimensional analysis indicated that …

    embry-riddle Repository record for Design and Numerical Evaluation of a Counter- Rotating Compressor in the Absence of Boundary Layer Control: Part II (opens in a new tab)

  5. Validation of interpolative interfaces for rotorcraft applications

    … and wind tunnel data. Tenasi is an unstructured, Reynolds Averaged Navier-Stokes (RANS) solver developed at the SimCenter: National Center for Computational Engineering, located at the University of Tennessee at Chattanooga. Steady-state results for the isolated ROBIN fuselage and unsteady results …

    utc Repository record for Validation of interpolative interfaces for rotorcraft applications (opens in a new tab)

  6. Large Eddy Simulation Based Turbulent Flow-induced Vibration of Fully Developed Pipe Flow

    … Commercial FSI software packages are based on Reynolds Averaged Navier-Stokes (RANS) fluid models, which do not compute the instantaneous fluctuations in turbulent flow. This thesis presents an FSI approach based on Large Eddy Simulation (LES) flow models, which do compute the instantaneous …

    byu Repository record for Large Eddy Simulation Based Turbulent Flow-induced Vibration of Fully Developed Pipe Flow (opens in a new tab)

  7. Machine Learning and Field Inversion approaches to Data-Driven Turbulence Modeling

    … need for improved closure models for the Reynolds-averaged Navier-Stokes (RANS) equations. This dissertation explores two different approaches for using experimental data to provide improved closure for the Reynolds stress tensor field. The first approach uses machine learning to learn a …

    vt Repository record for Machine Learning and Field Inversion approaches to Data-Driven Turbulence Modeling (opens in a new tab)

  8. Prediction of Noise Associated with an Isolated UAV Propeller

    … Simulation (LES) coupled with Unsteady Reynolds-Averaged Navier-Stokes (RANS) solver, is adopted on an isolated propeller modeled from the commercial DJI Phantom II 9450 propeller. The Spalart-Allmaras one equation turbulence model with rotation/curvature correction is used. The …

    embry-riddle Repository record for Prediction of Noise Associated with an Isolated UAV Propeller (opens in a new tab)

  9. Drag Reduction by Polymeric Additive Solutions

    … the evaluation of one of the newest viscoelastic Reynolds Averaged Navier-Stokes (RANS) turbulence models. Based on the k−ε−v 2−f framework, this model describes the viscoelastic effects of polymer additives using the Finitely Extensible Nonlinear Elastic-Peterlin (FENEP) constitutive model. To …

    vt Repository record for Drag Reduction by Polymeric Additive Solutions (opens in a new tab)

  10. Stabilized finite elements for compressible turbulent Navier-Stokes

    … solver for compressible turbulent flows. The Reynolds averaged Navier-Stokes (RANS) equations and modified Spalart-Almaras (SA) turbulence model are discretized using the streamline/upwind Petrov-Galerkin (SUPG) scheme. A fully implicit methodology is used to obtain steady state solutions or …

    utc Repository record for Stabilized finite elements for compressible turbulent Navier-Stokes (opens in a new tab)

  11. Modeling Outdoor Air Pollution and the Urban Form

    … thesis develops a solver for aerial pollutant transport by adding a passive-scalar transport equation to buoyantBoussinesqPimpleFoam, the OpenFOAM transient solver for buoyant, turbulent flow of incompressible fluids, with Reynolds Averaged Navier-Stokes (RANS) turbulence modeling. It then …

    mit Repository record for Modeling Outdoor Air Pollution and the Urban Form (opens in a new tab)

  12. Comparison of RANS Modeling to Dual-Plane PIV Measurements of the Turbulent Tip Vortex Trailed from a Hovering Rotor

    <p>Numerical simulations using the Reynolds-Averaged Navier-Stokes (RANS) equations were conducted to study the development and turbulent decay of the tip vortices in the wake produced by a hovering rotor. The computational results were compared to detailed, dual plane Particle Image Velocimetry …

    embry-riddle Repository record for Comparison of RANS Modeling to Dual-Plane PIV Measurements of the Turbulent Tip Vortex Trailed from a Hovering Rotor (opens in a new tab)

  13. Quantification of Spalart-Allmaras Turbulence Modeling Uncertainties for Hypersonic Flows Utilizing Output-Based Grid Adaptation

    … (SA) turbulence model with the compressible Reynolds-averaged Navier-Stokes (RANS) equations is quantified for steady non-reacting hypersonic flows using a coarse-grained uncertainty metric. Output-based adaptation is utilized to guarantee negligible numerical error with complex flow …

    mit Repository record for Quantification of Spalart-Allmaras Turbulence Modeling Uncertainties for Hypersonic Flows Utilizing Output-Based Grid Adaptation (opens in a new tab)

  14. Neural Operators for Learning Complex Nonlocal Mappings in Fluid Dynamics

    … tackles these challenges with a focus on Reynolds-Averaged Navier--Stokes (RANS) models, which will continue to serve as the backbone for many practical aircraft applications. Specifically, in RANS turbulence modeling, the challenges include developing more efficient ensemble filters to …

    vt Repository record for Neural Operators for Learning Complex Nonlocal Mappings in Fluid Dynamics (opens in a new tab)

  15. Computational analysis of plasma actuation for control of shock-laden flows in scramjet isolators

    Scramjets offer transformative capabilities for hypersonic propulsion, but are limited by instabilities associated with shock wave-boundary layer interactions (SWBLIs). These interactions can diminish engine performance and cause unstart, an aerodynamic phenomenon that can have catastrophic …

    uiuc Repository record for Computational analysis of plasma actuation for control of shock-laden flows in scramjet isolators (opens in a new tab)

  16. Adjoint-based optimization of U-bend channel flow using a multi-fidelity eddy viscosity turbulence model

    … to low-fidelity simulation methods, such as Reynolds Averaged Navier Stokes (RANS), due to current computational capabilities. However, RANS has been shown to lack sufficient accuracy for certain flows. This thesis presents CFD simulation of a 180 degree U-bend square duct using low-fidelity …

    mit Repository record for Adjoint-based optimization of U-bend channel flow using a multi-fidelity eddy viscosity turbulence model (opens in a new tab)

  17. Numerical prediction of the maneuvering characteristics of submarines operating near the free surface

    A method for coupling a Reynolds-averaged Navier-Stokes (RANS) computer code with an inviscid panel code to predict the maneuvering characteristics of submarines operating near the free-surface has been developed. The RANS code calculates the flow field immediately surrounding and in the wake of …

    mit Repository record for Numerical prediction of the maneuvering characteristics of submarines operating near the free surface (opens in a new tab)

  18. Predictive Turbulence Modeling with Bayesian Inference and Physics-Informed Machine Learning

    Reynolds-Averaged Navier-Stokes (RANS) simulations are widely used for engineering design and analysis involving turbulent flows. In RANS simulations, the Reynolds stress needs closure models and the existing models have large model-form uncertainties. Therefore, the RANS simulations are known to …

    vt Repository record for Predictive Turbulence Modeling with Bayesian Inference and Physics-Informed Machine Learning (opens in a new tab)

  19. An Assessment of the CFD Effectiveness for Simulating Wing Propeller Aerodynamics

    … aims to compare computational results from a Reynolds-Averaged Navier-Stokes (RANS) method, StarCCM+, and a vortex lattice method (VLM), VSP Aero. Two configurations that are analysed are 1) WIPP Configuration (Workshop for Integrated Propeller Prediction) 2) APROPOS Configuration. For WIPP, …

    vt Repository record for An Assessment of the CFD Effectiveness for Simulating Wing Propeller Aerodynamics (opens in a new tab)

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