|
![]() |
|||
|
||||
OverviewUses advanced structural theories to formulate and describe the coupling between finite elements and classical aerodynamic theories Aeroelasticity using the Finite Element Method deals with the Aeroelasticity of lifting bodies (wings and panels) by the Finite Element Method (FEM). It focuses on Aeroelasticity problems related to wings and panels: wings in subsonic range and panel in supersonic regime are treated. The structural models used are built by using classical and advanced one-dimensional (beams) and two-dimensional models (plates/shells) for the analysis of metallic and layered structures made by advanced composite materials. The elastic problems are formulated by means of finite element method. The aerodynamic fields and loadings are expressed by considering known theories used in classical aeroelasticity analysis: strip theory (in both steady and unsteady form), Theodorsen models, Vortex Lattice Method, Double Lattice Method and Piston Theory. Static and dynamic aeroelastic responses are both addressed. Static (divergence) and dynamic (flutter) response, including panel flutter are detailed in the book. * Formulates and describes the details of coupling between finite elements and classical aerodynamic theories. * Proposes advanced 1D and 2D structural FE models in a form similar to the formulation used in classical beam, plate, shell theories. These advanced theories permit exploration of aeroelastic phenomena that are not considered by classical theories. * Discusses classical aeroelasticity problems related to wings and panels. A valuable resource for Researchers in continuum mechanic of solids and structures Full Product DetailsAuthor: Erasmo Carrera , Marco Petrolo , Alberto Varello , Enrico ZappinoPublisher: John Wiley & Sons Inc Imprint: John Wiley & Sons Inc ISBN: 9781118337851ISBN 10: 1118337859 Pages: 256 Publication Date: 06 May 2022 Audience: Professional and scholarly , Professional & Vocational Format: Hardback Publisher's Status: Active Availability: Not yet available ![]() This item is yet to be released. You can pre-order this item and we will dispatch it to you upon its release. Table of ContentsReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |