AbstractFLUENT (a kind of CFD software) is applied to calculate the flow field in air-thrust bearings, and the thermodynamics characteristic and the statics characteristic are analyzed. In this paper, the governing equations of flow are Reynolds Averaging Navier-Stokes equation, and the model of turbulence is Realizable k-epsilon Model, in addition, enhanced wall treatment that combines a two-layer model with enhanced wall functions is employed
Computational analyses have been conducted on the Wall-mounted Glauert-Goldschmied type body ("hump"...
In this paper, an evolutionary algorithm is implemented for the purpose of performing symbolic regre...
Full seven-equation Reynolds stress turbulence models are promising tools for todays aerospace techn...
This paper presents a description and verification of RVC3D (rotor viscous code 3-D) which provides ...
Computational fluid dynamics (CFD) computations are performed at time increments using structural pr...
Following the consensus of a workshop in Turbulence Modeling for Liquid Rocket Thrust Chambers, the ...
The airflow around rockets with various nose cone and nozzle cone geometric parameters is investigat...
In the present work, the mixing of fuel and air in an isothermal high-intensity swirling flow in a m...
The objective of this research is to simulate steady and unsteady viscous flows, including rotor/sta...
Fully automated meshing for Reynolds-Averaged Navier-Stokes Simulations, Mesh generation for complex...
Launch Ascent and Vehicle Aerodynamics (LAVA) (Computational Fluid Dynamics (CFD) solver) contributi...
AbstractThe efficiency of mission varying aircrafts can be altered by either flow control method or ...
Four parts of the Reynolds-stress closure modeling are reported: (1) improvement of the k and epsilo...
This viewgraph presentation discusses the following: introduction to CFD Research Corporation; exper...
The fundamentals of large eddy simulation are considered and the approaches to it are compared. Subg...
Computational analyses have been conducted on the Wall-mounted Glauert-Goldschmied type body ("hump"...
In this paper, an evolutionary algorithm is implemented for the purpose of performing symbolic regre...
Full seven-equation Reynolds stress turbulence models are promising tools for todays aerospace techn...
This paper presents a description and verification of RVC3D (rotor viscous code 3-D) which provides ...
Computational fluid dynamics (CFD) computations are performed at time increments using structural pr...
Following the consensus of a workshop in Turbulence Modeling for Liquid Rocket Thrust Chambers, the ...
The airflow around rockets with various nose cone and nozzle cone geometric parameters is investigat...
In the present work, the mixing of fuel and air in an isothermal high-intensity swirling flow in a m...
The objective of this research is to simulate steady and unsteady viscous flows, including rotor/sta...
Fully automated meshing for Reynolds-Averaged Navier-Stokes Simulations, Mesh generation for complex...
Launch Ascent and Vehicle Aerodynamics (LAVA) (Computational Fluid Dynamics (CFD) solver) contributi...
AbstractThe efficiency of mission varying aircrafts can be altered by either flow control method or ...
Four parts of the Reynolds-stress closure modeling are reported: (1) improvement of the k and epsilo...
This viewgraph presentation discusses the following: introduction to CFD Research Corporation; exper...
The fundamentals of large eddy simulation are considered and the approaches to it are compared. Subg...
Computational analyses have been conducted on the Wall-mounted Glauert-Goldschmied type body ("hump"...
In this paper, an evolutionary algorithm is implemented for the purpose of performing symbolic regre...
Full seven-equation Reynolds stress turbulence models are promising tools for todays aerospace techn...