An aeroelastic model for composite rotor blades with straight and swept tips. I: Eroelastic stability in hover
type: Item
instance of: scholarly article
title: An aeroelastic model for composite rotor blades with straight and swept tips. I: Eroelastic stability in hover
zbMATH Open document ID: 1346.74019
DOI: 10.1016/S0020-7462(01)00109-3
author: P. P. Friedmann
author: Kuo-An Yuan
author: M. de Terlizzi
published in: International Journal of Non-Linear Mechanics
publication date: 2007-03-28T00:00:00Z
Mathematics Subject Classification ID: 74C99
Mathematics Subject Classification ID: 74F10
zbMATH DE Number: 5138081
MaRDI profile type: Publication
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description: scientific article; zbMATH DE number 5138081