Calculation of transonic flows around profiles with blunt and angled leading edges
Transonic flow is a mixed flow of subsonic and supersonic regions. Because of this mixture, the solution of transonic flow problems is obtained only when solving the differential equations of motion with special treatments for the transition from ...
Hoang Thi Bich Ngoc, Nguyen Manh Hung
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Loss Analysis of a Transonic Rotor with a Differential Approach to Entropy Generation
The loss mechanism of transonic axial compressors is a long-standing problem that involves almost all types of entropy generation in fluid flows, such as skin friction, shock waves, shear flows, corner separation, and tip vortices.
Jingyuan Ma, Feng Lin
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Numerical Solution of Compressible Steady Flows around the NACA 0012 Airfoil
The article presents results of a numerical solution of subsonic and transonic flows described by the system of Navier-Stokes equations in 2D laminar compressible flows around the NACA 0012 airfoil.
Kozel K, Kryštůfek P.
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Effect of Levels of Fidelity on Steady Aerodynamic and Static Aeroelastic Computations
Static aeroelastic deformations are nowadays considered as early as in the preliminary aircraft design stage, where low-fidelity linear aerodynamic modeling is favored because of its low computational cost.
Adrien Crovato +10 more
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Numerical Solution of Compressible Steady Flows around the RAE 2822 Airfoil
The article presents results of a numerical solution of subsonic, transonic and supersonic flows described by the system of Navier-Stokes equations in 2D laminar compressible flows around the RAE 2822 airfoil.
Kryštůfek P., Kozel K.
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Application of a fast transonic trajectory determination approach in 1-D modelling of steady-state two-phase carbon dioxide flow [PDF]
An original generalised procedure of determination of the transonic trajectory has been proposed. The procedure is much faster than the commonly used Newton Critical Point approach.
Angielczyk Wojciech +2 more
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Numerical study of the unsteady aerodynamics of helicopter rotor aerofoils
A two-dimensional model of the aerodynamics of rotor blades in forward flight is proposed in which the motion of the blade is represented by periodical variations of the freestrearn velocity and incidence. A novel implicit methodology for the solution
Shaw, Scott
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Numerical Solution of Inviscid Compressible Steady Flows around the RAE 2822 Airfoil
The article presents results of a numerical solution of subsonic, transonic and supersonic flows described by the system of Euler equations in 2D compressible flows around the RAE 2822 airfoil.
Kryštůfek P., Kozel K.
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A New High Resolution TVD Scheme for Unsteady Flows with Shock Waves
In this work, a new high resolution TVD scheme for unsteady flows with shock waves is presented. The performance of the scheme is investigated for solving Burgers and Euler’s equations.
R.A.B. Queiroz +2 more
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Numerical solution of compressible steady flows in a 2D GAMM channel and DCA 18% profile
The article presents results of a numerical solution of subsonic and transonic flows described by the system of Euler equations in 2D flows in a channel and around a profile.
Kozel Karel, Kryštůfek Pavel
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