Results 21 to 30 of about 9,803,992 (369)

MAESTROeX: A Massively Parallel Low Mach Number Astrophysical Solver [PDF]

open access: yesJournal of Open Source Software, 2019
We present MAESTROeX, a massively parallel solver for low Mach number astrophysical flows. The underlying low Mach number equation set allows for efficient, long-time integration for highly subsonic flows compared to compressible approaches. MAESTROeX is
Duoming Fan   +4 more
semanticscholar   +1 more source

Low Mach number limit on thin domains [PDF]

open access: yesNonlinearity, 2020
We consider the compressible Navier-Stokes system describing the motion of a viscous fluid confined to a straight layer $ _ =(0, )\times\mathbb{R}^2$. We show that the weak solutions in the 3D domain converge strongly to the solution of the 2D incompressible Navier-Stokes equations (Euler equations) when the Mach number $ $ tends to zero as well as
Caggio M.   +3 more
openaire   +4 more sources

Fuzzy-based prediction for suddenly expanded axisymmetric nozzle flows with microjets [PDF]

open access: yesBulletin of the Polish Academy of Sciences: Technical Sciences, 2022
The current research focuses on the implementation of the fuzzy logic approach for the prediction of base pressure as a function of the input parameters.
Jaimon D. Quadros   +5 more
doaj   +1 more source

On a diphasic low mach number system [PDF]

open access: yesESAIM: Mathematical Modelling and Numerical Analysis, 2005
The author proposes a diphasic low Mach number (DLMN) system for the modelling of diphasic flows at low Mach number. This system filters out the acoustic waves but keeps all the informations coming from the thermodynamic as the equations of state and the entropy contrary to a standard incompressible diphasic Navier-Stokes system.
Stéphane Dellacherie   +1 more
openaire   +2 more sources

Aeroengine High-Attitude/Low Mach Number Oscillations: Mechanism and Prevention Design

open access: yesInternational Journal of Aerospace Engineering, 2021
The issue of aeroengine oscillations over high-attitude and low-speed flight envelope has been an unsolved problem due to their classified nature and hard reproduction in simulated altitude test stand.
Jiqiang Wang
doaj   +1 more source

Theory Helps Observations: Determination of the Shock Mach Number and Scales From Magnetic Measurements

open access: yesFrontiers in Physics, 2022
The Mach number is one of the key parameters of collisionless shocks. Understanding shock physics requires knowledge of the spatial scales in the shock transition layer.
Michael Gedalin   +3 more
doaj   +1 more source

Low Mach number limit of some staggered schemes for compressible barotropic flows [PDF]

open access: yesMathematics of Computation, 2018
In this paper, we study the behaviour at low Mach number of numerical schemes based on staggered discretizations for the barotropic Navier-Stokes equations.
R. Herbin, J. Latché, Khaled Saleh
semanticscholar   +1 more source

Numerical Study on the Biomimetic Trailing Edge of a Turbine Blade Under a Wide Range of Outlet Mach Numbers

open access: yesFrontiers in Energy Research, 2021
This study was carried out to investigate the loss mechanism of a blade with a harbor seal whisker structure on the trailing edge under different Mach numbers.
Fengbo Wen   +4 more
doaj   +1 more source

An all Mach number relaxation upwind scheme

open access: yes, 2020
The present paper concerns the derivation of finite volume methods to approximate the weak solutions of the Euler equations within all Mach number regimes. To address such an issue, we develop a Suliciu relaxation type scheme.
C. Berthon, C. Klingenberg, Markus Zenk
semanticscholar   +1 more source

Flutter analysis of tapered composite fins: Analysis and experiment [PDF]

open access: yesFME Transactions, 2022
In the present work, the aeroelastic stability of tapered composite plates is investigated. Existing flutter models, based on the typical section approach, are reviewed for quasi-steady and unsteady low Mach number axial flows and modified for the thin ...
Dinulović Mirko   +3 more
doaj   +1 more source

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