#
Euler equations of motion
Resource Information
The concept ** Euler equations of motion** represents the subject, aboutness, idea or notion of resources found in **Houston Public Library**.

The Resource
Euler equations of motion
Resource Information

The concept

**Euler equations of motion**represents the subject, aboutness, idea or notion of resources found in**Houston Public Library**.- Label
- Euler equations of motion

- Source
- nasat

## Context

Context of Euler equations of motion#### Subject of

- 3-D unstructured method for flows past bodies in 6-DOF relative motion : preprint from proceedings of 6th International Symposium of Computational Fluid Dynamics, Japan Society of Computational Fluid Dynamics, September 4-8, 1995, Lake Tahoe, Nevada
- A Cartesian, cell-based approach for adaptively-refined solutions of the Euler and Navier-Stokes equations
- A Note on singularities of the 3-D Euler equation
- A coupled Eulerian/Lagrangian method for the solution of three-dimensional vortical flows
- A final report on NASA grant NSG 3079 entitled A linearized Euler analysis of unsteady flows in turbomachinery
- A genuinely multi-dimensional upwind cell-vertex scheme for the Euler equations
- A minimum entrophy principle in the gas dynamics equations
- A mixed volume grid approach for the Euler and Navier-Stokes equations
- A modified restricted Euler equation for turbulent flows with mean velocity gradients
- A multiblock multigrid three-dimensional Euler equation solver
- A perspective on unstructured grid flow problem solvers
- A simulation of rotor-stator interaction using the Euler equations and patched grids
- A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows : under contract NAS3-26618
- A zonal approach for prediction of jet noise
- Accuracy of schemes for the Euler equations with nonuniform meshes
- Adaptive grid embedding for the two-dimensional flux-split Euler equations
- Aerodynamics of engine-airframe interaction : final report
- Agglomeration multigrid for viscous turbulent flows
- An LU implicit scheme for high speed inlet analysis
- An LU-SSOR scheme for the Euler and Navier-Stokes equations
- An accuracy assessment of Cartesian-mesh approaches for the Euler equations
- An adaptively-refined, Cartesian cell-based scheme for the Euler and Navier-Stokes equations
- An analysis of rotor blade twist variables associated with different Euler sequences and pretwist treatments
- An approach to the development of numerical algorithms for first order linear hyperbolic systems in multiple space dimensions : the constant coefficient case
- An approximate method for calculating three-dimensional inviscid hypersonic flow fields
- An assessment of the adaptive unstructured tetrahedral grid, Euler flow solver code FELISA
- An assessment of viscous effects in computational simulation of benign and burst vortex flows on generic fighter wind-tunnel models using TEAM code
- An automated code generator for three-dimensional acoustic wave propagation with geometrically complex solid wall boundaries
- An efficient method for solving the steady Euler equations
- An implicit, conservative, zonal-boundary scheme for Euler equation calculations
- An multigrid LU-SSOR scheme for approximate Newton iteration applied to the Euler equations
- Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flows : final report for the period February 1988 to November 1988
- Application of an efficient hybrid scheme for aeroelastic analysis of advanced propellers
- Application of the space-time conservation element and solution element method to shock-tube problem
- Assessment of an Euler-interacting boundary layer method using high Reynolds number transonic transport flight data
- Boundary conditions for unsteady compressible flows
- Comparison of computational aeroacoustics prediction of acoustic transmission through a 3D stator with experiment
- Connection between the lattice Boltzmann equation and the beam scheme
- Contribution to the optimal shape design of two-dimensional internal flows with embedded shocks
- Control theory based airfoil design using the Euler equations
- Courant number and mach number insensitive CE/SE euler solvers
- Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing
- Development of a grid-independent approximate Riemann solver
- Development of a linearized unsteady Euler analysis for turbomachinery blade rows
- Development of a linearized unsteady Euler analysis with application to wake/blade-row interactions
- Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver
- Development of an aeroelastic code based on an Euler/Navier-Stokes aerodynamic solver
- Development of upwind schemes for the Euler equations
- Effect of density gradients in confined supersonic shear layers
- Effects of a forward-swept front rotor on the flowfield of a counterrotation propeller
- Efficient implementation of weighted ENO schemes
- Eigenmode analysis of boundary conditions for the one-dimensional preconditioned Euler equations
- Eigenmode analysis of unsteady one-dimensional Euler equations
- Embedding methods for the steady Euler equations
- Entropy analysis of kinetic flux vector splitting schemes for the compressible Euler equations
- Entropy jump across an inviscid shock wave
- Error estimates for cell-vertex solutions of the compressible Euler equations
- Euler and Navier-Stokes computations for two-dimensional geometries using unstructured meshes
- Euler flow predictions for an oscillating cascade using a high resolution wave-split scheme
- Euler solutions to nonlinear acoustics of non-lifting hovering rotor blades
- Euler solutions using an implicit multigrid technique
- Euler technology assessment for preliminary aircraft design : unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration
- Euler technology assessment for preliminary aircraft design employing OVERFLOW code with multiblock structured-grid method
- Euler technology assessment program for preliminary aircraft design employing SPLITFLOW code with cartesian unsructured grid method
- Evaluation of a doubly-swept blade tip for rotorcraft noise reduction
- Explicit and implicit compact high-resolution shock-capturing methods for multidimensional Euler equations I, formulation
- Factorizable schemes for the equations of fluid flow
- Final report of investigation of source location determination from Magsat magnetic anomalies : The Euler method approach (NCC 5-70)
- Final report on adaptive computational methods for SSME internal flow analysis
- Flow instabilities in transonic small disturbance theory
- Flow prediction for propfan engine installation effects on transport aircraft at transonic speeds
- Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver
- Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver
- High resolution schemes and the entropy condition
- High speed corner and gap seal computations using an LU-SGS scheme
- Implementation of a parallel unstructured Euler solver on the CM-5
- Implicit multigrid algorithms for the three-dimensional flux split Euler equations
- Implicit schemes and parallel computing in unstructured grid CFD
- Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems : final report, Task 1, Ducted propfan analysis
- Investigation of convection and pressures treatment with splitting techniques
- Marching iterative methods for the parabolized and thin layer Navier-Stokes equations
- Methodology for simulation of unsteady flows to determine the time-dependent interference between stationary and moving boundaries : [abstract
- Minimum time attitude slewing maneuvers of a rigid spacecraft
- Multigrid calculation of three-dimensional turbomachinery flows
- Multigrid methods for aerodynamic problems in complex geometries : final report
- New developments in the method of space-time conservation element and solution element-applications to two-dimensional time-marching problems
- Nonlinear (time domain) and linearized (title & freqency domain) solutions to the compressible Euler equations in conservation law form : final report for NASA Lewis Research Center
- Nonlinear acoustic wave propagation in atmosphere : final report, October 1, 1984 through October 31, 1985
- On absorbing boundary conditions for linearized Euler equations by a perfectly matched layer
- On bi-grid local mode analysis of solution techniques for 3-D Euler and Navier-Stokes equations
- On the Lagrangian method for steady and unsteady flow
- On the numerical solution of the dynamically loaded hydrodynamic lubrication of the point contact problem
- Optimum transonic airfoils based on the Euler equations
- Parallel implementation of the discontinuous Galerkin method
- Perfectly matched layer for linearized Euler equations in open and ducted domains
- Periodic time-domain nonlocal nonreflecting boundary conditions for duct acoustics
- Periodic time-domain nonlocal nonreflecting boundary conditions for duct acoustics
- Preliminary investigation of stability of a fin-stiffened slender strut
- Pressure updating methods for the steady-state fluid equations
- Progressive wave expansions and open boundary problems
- Pseudo-time method for optimal shape design using the Euler equations
- Research applied to transonic compressors in numerical fluid mechanics of inviscid flow and viscous flow : final technical report for Grant no. NAG 3-9 submitted to the NASA Lewis Research Center, Cleveland, OH 44135
- Shock wave interaction with an abrupt area change
- Solution-adaptive Cartesian cell approach for viscous and inviscid flows
- Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations
- Spectral methods for the Euler equations : Fourier methods and shock-capturing
- Stable boundary conditions and difference schemes for Navier-Stokes equations
- Stable boundary conditions for Cartesian grid calculations
- Supersonic wing and wing-body shape optimization using an adjoint formulation
- Technique for a very high order nonlinear simulation and validation
- Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes
- Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations
- The analysis and construction of perfectly matched layers for linearized Euler equations
- The construction and use of divergence free vector expansions for incompressible fluid flow calculations : [final report]
- The method of space-time conservation element and solution element-applications to one-dimensional and two-dimensional time-marching flow problems
- The space-time conservation element and solution element method--a new high-resolution and genuinely multidimensional paradigm for solving conservation laws, II, Numerical simulation of shock waves and contact discontinuities
- The upwind control volume scheme for unstructured triangular grids
- Three-dimensional Euler time accurate simulations of fan rotor-stator interactions
- Three-dimensional unsteady Euler euqation solutions using flux vector splitting
- Unstructured grid Euler method assessment for longitudinal and lateral/directional aerodynamic performance analysis of the HSR technology concept airplane at supersonic cruise speeds
- Unstructured grid Euler method assessment for longitudinal and lateral/directional stability analysis of the HSR Reference H configuration at transonic speeds
- Unstructured grid Euler method assessment for longitudinal and lateral/directional stability analysis of the HSR Reference H configuration at transonic speeds
- User's guide for ECAP2D : an Euler unsteady aerodynamic and aeroelastic analysis program for two dimensional oscillating cascades
- User's guide for ENSAERO--a multidisciplinary program for fluid/structural/control interaction studies of aircraft (release 1)
- User's manual for DuctE3D : a program for 3D Euler unsteady aerodynamic and aeroelastic analysis of ducted fans
- Variational methods in sensitivity analysis and optimization for aerodynamic applications : progress report for the period ended June 30, 1996 ... under research grant NCC1-68
- Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
- Zonal multigrid solution of compressible flow problems on unstructured and adaptive meshes

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