Journal ArticleDOI
Aeroelastic tailoring - Theory, practice, and promise
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TLDR
Aeroelastic tailoring technology is reviewed with reference to the historical background, underlying theory, current trends, and specific applications as mentioned in this paper, and the future of aero-linear tailoring and the development of an automated strength-aero-elastic design tool under the Automated Strength-AeroELastic Design program are examined.Abstract:
Aeroelastic tailoring technology is reviewed with reference to the historical background, the underlying theory, current trends, and specific applications. The specific application discussed include the Transonic Aircraft Technology program, an Advanced Design Composite Aircraft, the Wing/Inlet Advanced Development program, and the forward-swept wing. Finally, the future of aeroelastic tailoring and the development of an aeroelastic tailoring analysis and design tool under the Automated Strength-Aeroelastic Design program are examined.read more
Citations
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Journal ArticleDOI
Multidisciplinary Aerospace Design Optimization: Survey of Recent Developments
TL;DR: A survey of recent publications in the field of aerospace where interest in MDO has been particularly intense is presented, focused on the interaction of the structures discipline with other disciplines.
Proceedings ArticleDOI
Multidisciplinary aerospace design optimization: Survey of recent developments
TL;DR: A survey of recent publications in the field of aerospace where interest in multidisciplinary optimization has been particularly intense can be found in this paper, which includes sections on Mathematical Modeling, Design-oriented Analysis, Approximation Concepts, Optimization Procedures, System Sensitivity and Human Interface.
Journal ArticleDOI
Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow
TL;DR: In this paper, a model for a complete aircraft in subsonic flow is presented and validated for the Goland wing and the results give insight into various nonlinear aeroelastic phenomena of interest: 1) the effect of steadystate lift and accompanying deformation on the speed at which instabilities occur, 2) the effects on nonlinearities in limiting the amplitude of oscillations once an instability is encountered, and 3) the destabilizing effects of nonlinearity for finite disturbances at stable conditions.
Journal ArticleDOI
Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring
TL;DR: In this paper, flexible wing structures with geometric twist (adaptive washout for gust rejection, delayed stall) and aerodynamic twist for high lift, larger stability margins are both considered.
Journal ArticleDOI
Aeroelasticity of Nonconventional Airplane Configurations-Past and Future
Eli Livne,Terrence A. Weisshaar +1 more
TL;DR: In this article, the history of nonconventional airplane cone gurations is used to review some of the steps taken during the past century to establish aeroelastic effects as integrated design features that must be anticipated, controlled, and exploited.
References
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Book ChapterDOI
Introduction To Composite Materials
TL;DR: The combination of materials to form a new material system with enhanced material properties is a well documented historical fact as discussed by the authors, which is why many artisans from the Mediterranean and Far East used a form of composite technology in molding art works which were fabricated by layering cut paper in various sizes for producing desired shapes and contours.
Book
Introduction to composite materials
Stephen W. Tsai,H. Thomas Hahn +1 more
TL;DR: In this paper, the authors present a reference record created on 2005-11-18, modified on 2016-08-08 and used for Laminage Reference Record created on 2006-11/18.
Journal ArticleDOI
Structural synthesis - Its genesis and development
TL;DR: An historical account is given of the development, from its conception in 1960, of the structural synthesis method, and such elementary applications of synthesis methods as the three-bar truss, an integrally stiffened waffle plate, a stiffened cylindrical shell, and an idealized delta wing are given.
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