Reduced order unsteady aerodynamic modeling for stability and control analysis using computational fluid dynamics

M Ghoreyshi, A Jirásek, RM Cummings - Progress in Aerospace Sciences, 2014 - Elsevier
Recent advances and challenges in the generation of reduced order aerodynamic models
using computational fluid dynamics are presented. The models reviewed are those that can …

[图书][B] Riemann solvers and numerical methods for fluid dynamics: a practical introduction

EF Toro - 2013 - books.google.com
In 1917, the British scientist LF Richardson made the first reported attempt to predict the
weather by solving partial differential equations numerically, by hand! It is generally …

[图书][B] Computational fluid mechanics and heat transfer

D Anderson, JC Tannehill, RH Pletcher, R Munipalli… - 2020 - taylorfrancis.com
Computational Fluid Mechanics and Heat Transfer, Fourth Edition is a fully updated version
of the classic text on finite-difference and finite-volume computational methods. Divided into …

SPH and Riemann solvers

JJ Monaghan - Journal of Computational Physics, 1997 - Elsevier
Smooth particle hydrodynamics (SPH) is usually based on equations derived from the
momentum and thermal energy equations of fluid dynamics. Artificial viscosity is added to …

Relaxation of energy and approximate Riemann solvers for general pressure laws in fluid dynamics

F Coquel, B Perthame - SIAM Journal on Numerical Analysis, 1998 - SIAM
We consider the Euler equations for a compressible inviscid fluid with a general pressure
law p(ρ,ε), where ρ represents the density of the fluid and ε its specific internal energy. We …

Detached-eddy simulation with compressibility corrections applied to a supersonic axisymmetric base flow

JR Forsythe, KA Hoffmann… - J. Fluids …, 2002 - asmedigitalcollection.asme.org
Detached-eddy simulation is applied to an axisymmetric base flow at supersonic conditions.
Detached-eddy simulation is a hybrid approach to modeling turbulence that combines the …

Large-eddy simulation of a supersonic boundary layer using an unstructured grid

G Urbin, D Knight - AIAA journal, 2001 - arc.aiaa.org
MOST studies using large-eddy simulation (LES) have mainly focused on
incompressibleand subsonic ows. 1 In addition, most LES codes employ structured meshes …

Linearly implicit Rosenbrock-type Runge–Kutta schemes applied to the Discontinuous Galerkin solution of compressible and incompressible unsteady flows

F Bassi, L Botti, A Colombo, A Ghidoni, F Massa - Computers & Fluids, 2015 - Elsevier
In this work we investigate the use of linearly implicit Rosenbrock-type Runge–Kutta
schemes to integrate in time high-order Discontinuous Galerkin space discretizations of the …

Kestrel--A Fixed Wing Virtual Aircraft Product of the CREATE Program

SA Morton, B Tillman, DR McDaniel… - 2009 DoD High …, 2009 - ieeexplore.ieee.org
This paper documents a new integrating product that allows cross-over between simulation
of aerodynamics, dynamic stability and control, structures, propulsion, and store separation …

On postshock oscillations due to shock capturing schemes in unsteady flows

M Arora, PL Roe - Journal of Computational Physics, 1997 - Elsevier
In this paper, the issue of postshock oscillations generated by shock-capturing schemes is
investigated. Although these oscillations are frequently small enough to be ignored, there …