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Computational Methods For Fluid Dynamics by Ferziger%2c Joel H
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1DTIC ADA451870: The Implementation Of Probabilistic Methods For Uncertainty Analysis In Computational Fluid Dynamics Simulations Of Fluid Flow And Heat Transfer In A Gas Turbine Engine
By Defense Technical Information Center
Probabilistic methods have been implemented with a computational fluid dynamics simulation of fluid flow and heat transfer in a gas turbine engine. The simulation models the temperatures in the T-56 series III 1-2 spacer. Three input quantities are treated as random variables. A random sampling method is used to generate the input values from a probability density function. The implemented Monte Carlo method uses a large number of samples of the input variables to calculate results repeatedly for the output variables (i.e. the predicted temperatures). Statistics of the predicted temperatures, such as the mean and variance, are then calculated. The variation in the predicted temperature at one point in the turbine of the T56 engine is seen to be more sensitive to variability in some parameters than in others.
“DTIC ADA451870: The Implementation Of Probabilistic Methods For Uncertainty Analysis In Computational Fluid Dynamics Simulations Of Fluid Flow And Heat Transfer In A Gas Turbine Engine” Metadata:
- Title: ➤ DTIC ADA451870: The Implementation Of Probabilistic Methods For Uncertainty Analysis In Computational Fluid Dynamics Simulations Of Fluid Flow And Heat Transfer In A Gas Turbine Engine
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA451870: The Implementation Of Probabilistic Methods For Uncertainty Analysis In Computational Fluid Dynamics Simulations Of Fluid Flow And Heat Transfer In A Gas Turbine Engine” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Faragher, John - DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION VICTORIA (AUSTRALIA) AIR VEHICLES DIV - *HEAT TRANSFER - *COMPUTERIZED SIMULATION - *FLUID FLOW - *COMPUTATIONAL FLUID DYNAMICS - TEMPERATURE - MONTE CARLO METHOD - GAS TURBINES - AUSTRALIA - SAMPLING - PROBABILITY DENSITY FUNCTIONS - UNCERTAINTY - AIRCRAFT ENGINES - RANDOM VARIABLES
Edition Identifiers:
- Internet Archive ID: DTIC_ADA451870
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The book is available for download in "texts" format, the size of the file-s is: 18.59 Mbs, the file-s for this book were downloaded 45 times, the file-s went public at Mon Jun 04 2018.
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2DTIC ADA193891: Computational Fluid Dynamics Methods For Low Reynolds Number Precessing/Spinning Incompressible Flows
By Defense Technical Information Center
Three dimensional, steady-state, laminar, fully viscous Navier-Stokes simulations were used to predict the behavior of incompressible liquids that were undergoing steady spin and steady precession at a fixed precession angle. These numerical simulations can predict steady viscous and pressure moments. These moments tend to increase the precession angle and reduce the spin rate of the container system. For a completely filled cylinder, liquid-induced roll and side (yaw) moments were computed as functions of cylinder height to diameter. Keywords: Finite difference, Incompressible flow, Liquid-filled projectile, Liquid moment, Low reynolds number, Rotating liquids.
“DTIC ADA193891: Computational Fluid Dynamics Methods For Low Reynolds Number Precessing/Spinning Incompressible Flows” Metadata:
- Title: ➤ DTIC ADA193891: Computational Fluid Dynamics Methods For Low Reynolds Number Precessing/Spinning Incompressible Flows
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA193891: Computational Fluid Dynamics Methods For Low Reynolds Number Precessing/Spinning Incompressible Flows” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Nusca, Michael J - ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD - *NUMERICAL ANALYSIS - *SPINNING(MOTION) - *NAVIER STOKES EQUATIONS - *REYNOLDS NUMBER - *INCOMPRESSIBLE FLOW - *LIQUID FILLED PROJECTILES - *PRECESSION - SIMULATION - ANGLES - STEADY STATE - DIAMETERS - COMPUTATIONS - YAW - LIQUIDS - RATES - MOMENTS - FINITE DIFFERENCE THEORY - CYLINDRICAL BODIES - PRESSURE - CONTAINERS - NUMERICAL METHODS AND PROCEDURES - FLUID DYNAMICS - ROTATION - VISCOUS FLOW - VISCOSITY - LOW RATE - HEIGHT - FILLING - INCOMPRESSIBILITY
Edition Identifiers:
- Internet Archive ID: DTIC_ADA193891
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The book is available for download in "texts" format, the size of the file-s is: 18.25 Mbs, the file-s for this book were downloaded 58 times, the file-s went public at Sun Feb 18 2018.
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3DTIC ADA221946: Computational Methods For Problems In Fluid Dynamics
By Defense Technical Information Center
The research reported herein addresses the reduced basis method, which is based on the combination of a basic iteractive method and a projection method. The convergence is analyzed and some error bounds are established. The relationship between the reduced basis method and the preconditioned conjugate gradient method is discussed. Also included is a practical implementation of the reduced basis method when a pseudoresidual-based Krylov space is chosen. The final section of this report dwells on the weight selection procedures of hybrid difference methods for the linear convective equation. The procedures are based on the ability of hybrid difference methods to conserve the discrete weighted energy. Keywords: Reduced basis; Linear solver; Contraction number; Projection method; Sparse symmetric linear systems; Hybrid difference methods.
“DTIC ADA221946: Computational Methods For Problems In Fluid Dynamics” Metadata:
- Title: ➤ DTIC ADA221946: Computational Methods For Problems In Fluid Dynamics
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA221946: Computational Methods For Problems In Fluid Dynamics” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Chou, So-Hsiang - BOWLING GREEN STATE UNIV OH DEPT OF MATHEMATICS - *FLUID DYNAMICS - *NUMERICAL METHODS AND PROCEDURES - ENERGY - CONVECTION - WEIGHTING FUNCTIONS - LINEAR ALGEBRAIC EQUATIONS - HYBRID SYSTEMS - SELECTION - GRADIENTS - LINEAR SYSTEMS - ALGORITHMS - SYMMETRY
Edition Identifiers:
- Internet Archive ID: DTIC_ADA221946
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The book is available for download in "texts" format, the size of the file-s is: 13.36 Mbs, the file-s for this book were downloaded 54 times, the file-s went public at Sun Feb 25 2018.
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4NASA Technical Reports Server (NTRS) 20170003036: On High-Order Space-Time Methods For Computational Fluid Dynamics (CFD)
By NASA Technical Reports Server (NTRS)
High-order space-time methods for Computational Fluid Dynamics are studied. Both explicit and implicit schemes will be discussed
“NASA Technical Reports Server (NTRS) 20170003036: On High-Order Space-Time Methods For Computational Fluid Dynamics (CFD)” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 20170003036: On High-Order Space-Time Methods For Computational Fluid Dynamics (CFD)
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 20170003036: On High-Order Space-Time Methods For Computational Fluid Dynamics (CFD)” Subjects and Themes:
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_20170003036
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5NASA Technical Reports Server (NTRS) 20140002886: High-Order Methods For Computational Fluid Dynamics: A Brief Review Of Compact Differential Formulations On Unstructured Grids
By NASA Technical Reports Server (NTRS)
Popular high-order schemes with compact stencils for Computational Fluid Dynamics (CFD) include Discontinuous Galerkin (DG), Spectral Difference (SD), and Spectral Volume (SV) methods. The recently proposed Flux Reconstruction (FR) approach or Correction Procedure using Reconstruction (CPR) is based on a differential formulation and provides a unifying framework for these high-order schemes. Here we present a brief review of recent developments for the FR/CPR schemes as well as some pacing items.
“NASA Technical Reports Server (NTRS) 20140002886: High-Order Methods For Computational Fluid Dynamics: A Brief Review Of Compact Differential Formulations On Unstructured Grids” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 20140002886: High-Order Methods For Computational Fluid Dynamics: A Brief Review Of Compact Differential Formulations On Unstructured Grids
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 20140002886: High-Order Methods For Computational Fluid Dynamics: A Brief Review Of Compact Differential Formulations On Unstructured Grids” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - COMPUTATIONAL FLUID DYNAMICS - GALERKIN METHOD - UNSTRUCTURED GRIDS (MATHEMATICS) - RUNGE-KUTTA METHOD - SPECTRAL METHODS - DIFFERENTIAL EQUATIONS - Huynh, H. T. - Wang, Z. J. - Vincent, P. E.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_20140002886
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The book is available for download in "texts" format, the size of the file-s is: 17.41 Mbs, the file-s for this book were downloaded 60 times, the file-s went public at Mon Nov 14 2016.
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6Computational Methods For Fluid Dynamics
By Ferziger, Joel H and Peric, M. (Milovan), 1957-
Includes bibliographical references (p. [353]-361) and index
“Computational Methods For Fluid Dynamics” Metadata:
- Title: ➤ Computational Methods For Fluid Dynamics
- Authors: Ferziger, Joel HPeric, M. (Milovan), 1957-
- Language: English
“Computational Methods For Fluid Dynamics” Subjects and Themes:
- Subjects: Fluid dynamics - Fluides, Dynamique des - Strömungsmechanik - Numerisches Verfahren
Edition Identifiers:
- Internet Archive ID: computationalmet00ferz
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7DTIC ADA223935: Technical Evaluation Report On The Fluid Dynamics Panel Symposium On Computational Methods For Aerodynamic Design (Inverse) And Optimization (Les Methodes De Calcul Pour La Conception Aerodynamique (Methodes Inverses) Et L'Optimisation)
By Defense Technical Information Center
The papers presented at the AGARD Fluid Dynamics Panel Specialists' Meeting on 'Computational Methods for Aerodynamic Design (Inverse) and Optimization' are reviewed. Strengths and weaknesses are identified for many of the contributions as each is reviewed. The reviewer closes with some general comments. The 23 papers presented at the Meeting have been collected in AGARD CP 463 (ADA220870). Keywords: Computer aided design; Computational fluid dynamics; Inverse methods; Aerodynamic characteristics/optimization.
“DTIC ADA223935: Technical Evaluation Report On The Fluid Dynamics Panel Symposium On Computational Methods For Aerodynamic Design (Inverse) And Optimization (Les Methodes De Calcul Pour La Conception Aerodynamique (Methodes Inverses) Et L'Optimisation)” Metadata:
- Title: ➤ DTIC ADA223935: Technical Evaluation Report On The Fluid Dynamics Panel Symposium On Computational Methods For Aerodynamic Design (Inverse) And Optimization (Les Methodes De Calcul Pour La Conception Aerodynamique (Methodes Inverses) Et L'Optimisation)
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA223935: Technical Evaluation Report On The Fluid Dynamics Panel Symposium On Computational Methods For Aerodynamic Design (Inverse) And Optimization (Les Methodes De Calcul Pour La Conception Aerodynamique (Methodes Inverses) Et L'Optimisation)” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Henne, Preston A - ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE) - *AERODYNAMICS - *COMPUTATIONS - SYMPOSIA - OPTIMIZATION - COMPUTER AIDED DESIGN - AERODYNAMIC CHARACTERISTICS - INVERSION - NUMERICAL METHODS AND PROCEDURES - SPECIALISTS - FLUID DYNAMICS - PANEL(COMMITTEE) - METHODOLOGY - TEST AND EVALUATION - PANELS
Edition Identifiers:
- Internet Archive ID: DTIC_ADA223935
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8Numerical Methods For Fluid Dynamics III : Based On The Proceedings Of A Conference Organized By The Institute For Computational Fluid Dynamics Of The Universities Of Oxford And Reading In Association With The Institute Of Mathematics And [its] Applications On Numerical Methods For Fluid Dynamics, Held In Oxford In March 1988
By None
The papers presented at the AGARD Fluid Dynamics Panel Specialists' Meeting on 'Computational Methods for Aerodynamic Design (Inverse) and Optimization' are reviewed. Strengths and weaknesses are identified for many of the contributions as each is reviewed. The reviewer closes with some general comments. The 23 papers presented at the Meeting have been collected in AGARD CP 463 (ADA220870). Keywords: Computer aided design; Computational fluid dynamics; Inverse methods; Aerodynamic characteristics/optimization.
“Numerical Methods For Fluid Dynamics III : Based On The Proceedings Of A Conference Organized By The Institute For Computational Fluid Dynamics Of The Universities Of Oxford And Reading In Association With The Institute Of Mathematics And [its] Applications On Numerical Methods For Fluid Dynamics, Held In Oxford In March 1988” Metadata:
- Title: ➤ Numerical Methods For Fluid Dynamics III : Based On The Proceedings Of A Conference Organized By The Institute For Computational Fluid Dynamics Of The Universities Of Oxford And Reading In Association With The Institute Of Mathematics And [its] Applications On Numerical Methods For Fluid Dynamics, Held In Oxford In March 1988
- Author: None
- Language: English
“Numerical Methods For Fluid Dynamics III : Based On The Proceedings Of A Conference Organized By The Institute For Computational Fluid Dynamics Of The Universities Of Oxford And Reading In Association With The Institute Of Mathematics And [its] Applications On Numerical Methods For Fluid Dynamics, Held In Oxford In March 1988” Subjects and Themes:
- Subjects: ➤ Fluid dynamics -- Mathematics -- Congresses - Numerical calculations -- Congresses - Fluides, Dynamique des -- Mathématiques -- Congrès - Calculs numériques -- Congrès - Fluid dynamics -- Mathematics - Numerical calculations - Fluid dynamics Mathematics Congresses - Numerical calculations Congresses
Edition Identifiers:
- Internet Archive ID: numericalmethods0000unse
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9DTIC ADA264833: Computational Fluid Dynamics Research On Dynamically Adaptive Mesh Methods For Transonic Flows
By Defense Technical Information Center
Dynamic mesh adaptation strategies are investigated. These include software development, dynamically adaptive mesh schemes, errors arising from generalized mappings and orthogonality. The strategies developed are tested against the euler and viscous Burgers Equations.
“DTIC ADA264833: Computational Fluid Dynamics Research On Dynamically Adaptive Mesh Methods For Transonic Flows” Metadata:
- Title: ➤ DTIC ADA264833: Computational Fluid Dynamics Research On Dynamically Adaptive Mesh Methods For Transonic Flows
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA264833: Computational Fluid Dynamics Research On Dynamically Adaptive Mesh Methods For Transonic Flows” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Hindman, Richard G - IOWA STATE UNIV AMES - *COMPUTATIONAL FLUID DYNAMICS - *TRANSONIC FLOW - COMPUTER PROGRAMS - STRATEGY - ERRORS - NUMERICAL METHODS AND PROCEDURES - ADAPTATION - ORTHOGONALITY - FLUID DYNAMICS - EQUATIONS - FLUIDS - MESH - DYNAMICS
Edition Identifiers:
- Internet Archive ID: DTIC_ADA264833
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The book is available for download in "texts" format, the size of the file-s is: 31.38 Mbs, the file-s for this book were downloaded 67 times, the file-s went public at Sat Mar 10 2018.
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