Data-driven modeling for unsteady aerodynamics and aeroelasticity

J Kou, W Zhang - Progress in Aerospace Sciences, 2021 - Elsevier
Aerodynamic modeling plays an important role in multiphysics and design problems, in
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 …

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 …

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 …

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 …

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 …

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 …

[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 …

Harmonic balance methods applied to computational fluid dynamics problems

KC Hall, K Ekici, JP Thomas… - International Journal of …, 2013 - Taylor & Francis
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 …

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 …