Results 11 to 20 of about 1,283 (268)

A face-based immersed boundary method for compressible flows using a uniform interpolation stencil

open access: yesFrontiers in Mechanical Engineering, 2022
In this study, an immersed boundary method developed for compressible viscous flows (Ramakrishnan, R., Girdhar, A., & Ghosh, S. (2016). Immersed Boundary Methods for Compressible Laminar Flows) is modified to improve their stability and robustness ...
M. L. N. V. Kasturi Rangan   +1 more
doaj   +1 more source

Experimental results and numerical simulations for transonic flow over the ONERA M4R model [PDF]

open access: yesINCAS Bulletin, 2013
This paper presents a comparison between experimental results of transonic flow over the ONERA M4R calibration model obtained in the INCAS Trisonic wind tunnel and the numerical results.
Marius Gabriel COJOCARU   +5 more
doaj   +1 more source

Numerical experiment with upstream boundary conditions

open access: yesEPJ Web of Conferences, 2012
The work deals with a numerical solution of subsonic and transonic flows described by the system of Euler equations in 2D and 3D flows in a channel. Authors used Lax-Wendroff and the multistage Runge-Kutta scheme to numerically solve the flows in a 2D G AMM
Huml Jaroslav, Kozel Karel
doaj   +1 more source

Loss Analysis of a Transonic Rotor with a Differential Approach to Entropy Generation

open access: yesMachines, 2023
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
doaj   +1 more source

Calculation of transonic flows around profiles with blunt and angled leading edges

open access: yesVietnam Journal of Mechanics, 2016
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
doaj   +1 more source

Numerical Solution of Compressible Steady Flows around the RAE 2822 Airfoil

open access: yesEPJ Web of Conferences, 2014
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.
doaj   +1 more source

Effect of Levels of Fidelity on Steady Aerodynamic and Static Aeroelastic Computations

open access: yesAerospace, 2020
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
doaj   +1 more source

Application of a fast transonic trajectory determination approach in 1-D modelling of steady-state two-phase carbon dioxide flow [PDF]

open access: yesE3S Web of Conferences, 2019
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
doaj   +1 more source

Smooth Transonic Flows Around Cones

open access: yesNetworks and Heterogeneous Media, 2022
<p style='text-indent:20px;'>We consider a conical body facing a supersonic stream of air at a uniform velocity. When the opening angle of the obstacle cone is small, the conical shock wave is attached to the vertex. Under the assumption of self-similarity for irrotational motions, the Euler system is transformed into the nonlinear ODE system. We
Lien, Wen-Ching   +2 more
openaire   +2 more sources

Numerical Solution of Compressible Steady Flows around the NACA 0012 Airfoil

open access: yesEPJ Web of Conferences, 2013
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.
doaj   +1 more source

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