Principles of Aeroelasticity

Principles of Aeroelasticity

Author: Raymond L. Bisplinghoff

Publisher: Courier Corporation

Published: 2013-10-17

Total Pages: 545

ISBN-13: 0486783162

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Geared toward professional engineers, this volume will be helpful for students, too. Topics include methods of constructing static and dynamic equations, heated elastic solids, forms of aerodynamic operators, structural operators, and more. 1962 edition.


Aeroelasticity

Aeroelasticity

Author: Raymond L. Bisplinghoff

Publisher: Addison Wesley Publishing Company

Published: 1955

Total Pages: 882

ISBN-13:

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Introduction to Aircraft Aeroelasticity and Loads

Introduction to Aircraft Aeroelasticity and Loads

Author: Jan R. Wright

Publisher: John Wiley & Sons

Published: 2007

Total Pages: 499

ISBN-13: 9780470858417

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"Introduction to Aircraft Aeroelasticity and Loads takes the readers up to a level where they will begin to understand the underlying aeroelastic and loads principles and procedures in a modern aircraft design office. It Is ideal for final year undergraduate and/or masters level students as well as engineers in Industry who are new to the field."--BOOK JACKET.


Introduction to Aeroelasticity

Introduction to Aeroelasticity

Author: Harijono Djojodihardjo

Publisher: Springer Nature

Published: 2023-09-03

Total Pages: 1080

ISBN-13: 9811680787

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This textbook is intended as a core text for courses on aeroelasticity or aero-elasto-mechanics for senior undergraduate/graduate programs in aerospace and mechanical engineering. The book focuses on the basic understanding of the concepts required in learning about aeroelasticity, from observation, reasoning, and understanding fundamental physical principles. Fundamental and simple mathematics will be introduced to describe the features of aeroelastic problems, and to devise simple concurrent physical and mathematical modeling. It will be accompanied by the introduction and understandings of the mechanisms that create the interactions that generate the aeroelastic phenomena considered. The students will also be led to the relation between observed phenomena, assumptions that may have to be adopted to arrive at physical and mathematical modelling, interpreting and verifying the results, and the accompanied limitations, uncertainties and inaccuracies. The students will also be introduced to combine engineering problem solving attitude and determination with simple mechanics problem-solving skills that coexist harmoniously with a useful mechanical intuition.


Principles of Aeroelasticity

Principles of Aeroelasticity

Author: Rama B. Bhat

Publisher: CRC Press

Published: 2016-04-27

Total Pages: 181

ISBN-13: 1498724736

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Introductory Guide on the Design of Aerospace Structures Developed from a course taught at Concordia University for more than 20 years, Principles of Aeroelasticity utilizes the author’s extensive teaching experience to immerse undergraduate and first-year graduate students into this very specialized subject. Ideal for coursework or self-study, this detailed examination introduces the concepts of aeroelasticity, describes how aircraft lift structures behave when subjected to aerodynamic loads, and finds its application in aerospace, civil, and mechanical engineering. The book begins with a discussion on static behavior, and moves on to static instability and divergence, dynamic behavior leading up to flutter, and fluid structure interaction problems. It covers classical approaches based on low-order aerodynamic models and provides a rationale for adopting certain aeroelastic models. The author describes the formulation of discrete models as well as continuous structural models. He also provides approximate methods for solving divergence, flutter, response and stability of structures, and addresses non-aeroelastic problems in other areas that are similar to aeroelastic problems. Topics covered include: The fundamentals of vibration theory Vibration of single degree of freedom and two degrees of freedom systems Elasticity in the form of an idealized spring element Repetitive motion Flutter phenomenon Classical methods, Rayleigh-Ritz techniques, Galerkin’s technique, influential coefficient methods, and finite element methods Unsteady aerodynamics, and more


Aeroelasticity

Aeroelasticity

Author: AV Balakrishnan

Publisher: Springer Science & Business Media

Published: 2012-07-12

Total Pages: 408

ISBN-13: 1461436095

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The author's approach is one of continuum models of the aerodynamic flow interacting with a flexible structure whose behavior is governed by partial differential equations. Both linear and nonlinear models are considered although much of the book is concerned with the former while keeping the latter clearly in view. A complete chapter is also devoted to nonlinear theory. The author has provided new insights into the classical inviscid aerodynamics and raises novel and interesting questions on fundamental issues that have too often been neglected or forgotten in the development of the early history of the subject. The author contrasts his approach with discrete models for the unsteady aerodynamic flow and the finite element model for the structure. Much of the aeroelasticity has been developed with applications formerly in mind because of its enormous consequences for the safety of aircraft. Aeroelastic instabilities such as divergence and flutter and aeroelastic responses to gusts can pose a significant hazard to the aircraft and impact its performance. Yet, it is now recognized that there are many other physical phenomena that have similar characteristics ranging from flows around flexible tall buildings and long span bridges, alternate energy sources such as electric power generation by smart structures to flows internal to the human body. From the foreword: "For the theorist and applied mathematician who wishes an introduction to this fascinating subject as well as for the experienced aeroelastician who is open to new challenges and a fresh viewpoint, this book and its author have much to offer the reader." Earl Dowell, Duke University, USA


Introduction to Structural Dynamics and Aeroelasticity

Introduction to Structural Dynamics and Aeroelasticity

Author: Dewey H. Hodges

Publisher: Cambridge University Press

Published: 2002-07-01

Total Pages: 186

ISBN-13: 9781139433914

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Aeroelastic and structural dynamic phenomena play an important role in many facets of engineering. In particular, an understanding of these disciplines is essential to the design of aircraft and space vehicles. This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity, and dynamic aeroelasticity. The structural dynamics material emphasizes vibration, the modal representation, and dynamic response. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter, and elastic tailoring. Both exact and approximate solution methodologies are stressed. More than one hundred illustrations and tables help clarify the text, while upwards of fifty problems enhance student learning.