Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Flutter Analysis of a supersonic composite AirFoil skin by using the Differential Quadrature Method
01.01.2012
12 pages
Aufsatz (Zeitschrift)
Englisch
DDC:
620.118
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime
British Library Online Contents | 2017
|Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime
British Library Online Contents | 2017
|Supersonic Panel Flutter Analysis Assuming Effects of Initial Structural Stresses
Springer Verlag | 2019
|Supersonic Panel Flutter Analysis Assuming Effects of Initial Structural Stresses
Online Contents | 2019
|