Nonlinear Aerodynamic Wing Design
Author : Ellwood Bonner
Publisher :
Page : 71 pages
File Size : 28,16 MB
Release : 1985
Category :
ISBN :
Author : Ellwood Bonner
Publisher :
Page : 71 pages
File Size : 28,16 MB
Release : 1985
Category :
ISBN :
Author :
Publisher :
Page : 84 pages
File Size : 35,6 MB
Release : 1985
Category :
ISBN :
Author : Harry W. Carlson
Publisher :
Page : 104 pages
File Size : 44,49 MB
Release : 1980
Category : Aerodynamics, Supersonic
ISBN :
Author : J. N. Reddy
Publisher : CRC Press
Page : 568 pages
File Size : 43,19 MB
Release : 1999-02-10
Category : Technology & Engineering
ISBN : 9781560327059
This text presents a complete treatment of the theory and analysis of elastic plates. It provides detailed coverage of classic and shear deformation plate theories and their solutions by analytical as well as numerical methods for bending, buckling and natural vibrations. Analytical solutions are based on the Navier and Levy solution method, and numerical solutions are based on the Rayleigh-Ritz methods and finite element method. The author address a range of topics, including basic equations of elasticity, virtual work and energy principles, cylindrical bending of plates, rectangular plates and an introduction to the finite element method with applications to plates.
Author : James C. Sivells
Publisher :
Page : 512 pages
File Size : 21,6 MB
Release : 1947
Category : Aerodynamics
ISBN :
A method is presented for calculating wing characteristics by lifting-line theory using nonlinear section lift data. Material from various sources is combined with some original work into the single complete method described.
Author :
Publisher :
Page : 18 pages
File Size : 13,36 MB
Release : 1991
Category :
ISBN :
Author :
Publisher :
Page : 88 pages
File Size : 24,38 MB
Release : 1980
Category :
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Author : M. A. Ferman
Publisher : Trafford Publishing
Page : 71 pages
File Size : 28,10 MB
Release : 2011
Category : Technology & Engineering
ISBN : 1426973101
"This wind design method is based on a technique the author originally developed for use in the aircraft industry, and modified to enhance usage for aerospace students, and more recently, home builders."--Introduction.
Author : Michail G. Michailidis
Publisher : Springer Nature
Page : 119 pages
File Size : 45,54 MB
Release : 2020-02-21
Category : Technology & Engineering
ISBN : 3030407160
This book introduces a comprehensive and mathematically rigorous controller design for families of nonlinear systems with time-varying parameters and unstructured uncertainties. Although the presented methodology is general, the specific family of systems considered is the latest, NextGen, unconventional fixed-wing unmanned aircraft with circulation control or morphing wings, or a combination of both. The approach considers various sources of model and parameter uncertainty, while the controller design depends not on a nominal plant model, but instead on a family of admissible plants. In contrast to existing controller designs that consider multiple models and multiple controllers, the proposed approach is based on the ‘one controller fits all models’ within the unstructured uncertainty interval. The book presents a modeling-based analysis and synthesis approach with additive uncertainty weighting functions for accurate realization of the candidate systems. This differs significantly from existing designs in that it is capable of handling time-varying characteristics. This research monograph is suitable for scientists, engineers, researchers and graduate students with a background in control system theory who are interested in complex engineering nonlinear systems.
Author : Grigorios Dimitriadis
Publisher : John Wiley & Sons
Page : 944 pages
File Size : 34,33 MB
Release : 2017-03-10
Category : Technology & Engineering
ISBN : 1118756460
Introduction to Nonlinear Aeroelasticity Introduces the latest developments and technologies in the area of nonlinear aeroelasticity Nonlinear aeroelasticity has become an increasingly popular research area in recent years. There have been many driving forces behind this development, increasingly flexible structures, nonlinear control laws, materials with nonlinear characteristics and so on. Introduction to Nonlinear Aeroelasticity covers the theoretical basics in nonlinear aeroelasticity and applies the theory to practical problems. As nonlinear aeroelasticity is a combined topic, necessitating expertise from different areas, the book introduces methodologies from a variety of disciplines such as nonlinear dynamics, bifurcation analysis, unsteady aerodynamics, non-smooth systems and others. The emphasis throughout is on the practical application of the theories and methods, so as to enable the reader to apply their newly acquired knowledge Key features: Covers the major topics in nonlinear aeroelasticity, from the galloping of cables to supersonic panel flutter Discusses nonlinear dynamics, bifurcation analysis, numerical continuation, unsteady aerodynamics and non-smooth systems Considers the practical application of the theories and methods Covers nonlinear dynamics, bifurcation analysis and numerical methods Accompanied by a website hosting Matlab code Introduction to Nonlinear Aeroelasticity is a comprehensive reference for researchers and workers in industry and is also a useful introduction to the subject for graduate and undergraduate students across engineering disciplines.