An application of finite Hilbert transforms in the derivation of a state space model for an aeroelastic system
type: Item
instance of: scholarly article
title: An application of finite Hilbert transforms in the derivation of a state space model for an aeroelastic system
zbMATH Open document ID: 0734.76006
author: Terry L. Herdman
author: Janos Turi
published in: Journal of Integral Equations and Applications
publication date: 1991-01-01T00:00:00Z
review text: Dynamic modelling of various aerolastic control systems (e.g., an airfoil) requires an application of Söhngen's inversion formula for finite Hilbert transforms. In order to justify the validity of the inversion formula it is shown that the circulation history must belong to a weighted \(L_ 2\) space.
Mathematics Subject Classification ID: 76B10
Mathematics Subject Classification ID: 44A15
zbMATH DE Number: 4215531
zbMATH Keywords: Dynamic modelling
zbMATH Keywords: aerolastic control systems
zbMATH Keywords: airfoil
zbMATH Keywords: Söhngen's inversion formula
zbMATH Keywords: Hilbert transforms
zbMATH Keywords: circulation
reviewed by: Søren Christiansen
MaRDI profile type: Publication
full work available at URL: https://doi.org/10.1216/jiea/1181075618
OpenAlex ID: W2047928323
DOI: 10.1216/JIEA/1181075618
description: scientific article; zbMATH DE number 4215531