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Data-driven modeling for unsteady aerodynamics and aeroelasticity
Aerodynamic modeling plays an important role in multiphysics and design problems, in
addition to experiment and numerical simulation, due to its low-dimensional representation …
addition to experiment and numerical simulation, due to its low-dimensional representation …
Reduced-order modeling: new approaches for computational physics
DJ Lucia, PS Beran, WA Silva - Progress in aerospace sciences, 2004 - Elsevier
In this paper, we review the development of new reduced-order modeling techniques and
discuss their applicability to various problems in computational physics. Emphasis is given …
discuss their applicability to various problems in computational physics. Emphasis is given …
Nonreflecting boundary conditions for Euler equation calculations
MB Giles - AIAA journal, 1990 - arc.aiaa.org
This paper presents a unified theory for the construction of steady-state and unsteady
nonreflecting boundary conditions for the Euler equations. These allow calculations to be …
nonreflecting boundary conditions for the Euler equations. These allow calculations to be …
A review of aeroelasticity methods with emphasis on turbomachinery applications
JG Marshall, M Imregun - Journal of fluids and structures, 1996 - Elsevier
This paper is a review of current aeroelasticity methods, with particular emphasis on
turbomachinery applications. It also includes a brief survey of the computational fluid …
turbomachinery applications. It also includes a brief survey of the computational fluid …
Fourier methods for turbomachinery applications
L He - Progress in Aerospace Sciences, 2010 - Elsevier
Rapid increase in computing power has made a huge difference in scales and complexities
of the problems in turbomachinery that we can tackle by use of computational fluid dynamics …
of the problems in turbomachinery that we can tackle by use of computational fluid dynamics …
A harmonic balance technique for multistage turbomachinery applications
C Frey, G Ashcroft, HP Kersken… - … Expo: Power for …, 2014 - asmedigitalcollection.asme.org
This article describes a nonlinear frequency domain method for the simulation of unsteady
blade row interaction problems across several blade rows in turbomachinery. The capability …
blade row interaction problems across several blade rows in turbomachinery. The capability …
Eigenanalysis of unsteady flows about airfoils, cascades, and wings
KC Hall - AIAA journal, 1994 - arc.aiaa.org
A general technique for constructing reduced order models of unsteady aerodynamic flows
about twodimensional isolated airfoils, cascades of airfoils, and three-dimensional wings is …
about twodimensional isolated airfoils, cascades of airfoils, and three-dimensional wings is …
[KIRJA][B] Non-reflecting boundary conditions for the Euler equations
M Giles - 1988 - people.maths.ox.ac.uk
When calculating a numerical solution to an unsteady, hyperbolic, partial di erential
equation on an in nite domain, it is normal to perform the calculation on a truncated nite …
equation on an in nite domain, it is normal to perform the calculation on a truncated nite …
Harmonic balance methods applied to computational fluid dynamics problems
In this paper, we briefly review the classical harmonic balance method, and describe the
adaptation of the method required for its application to computational fluid dynamics models …
adaptation of the method required for its application to computational fluid dynamics models …
A time-linearized Navier–Stokes analysis of stall flutter
WS Clark, KC Hall - J. Turbomach., 2000 - asmedigitalcollection.asme.org
A computational method for predicting unsteady viscous flow through two-dimensional
cascades accurately and efficiently is presented. The method is intended to predict the onset …
cascades accurately and efficiently is presented. The method is intended to predict the onset …