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Introduction to Structural Dynamics and Aeroelasticity, Hodges


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Цена: 8395.00р.
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Автор: Hodges
Название:  Introduction to Structural Dynamics and Aeroelasticity
ISBN: 9781107617094
Издательство: Cambridge Academ
Классификация:
ISBN-10: 110761709X
Обложка/Формат: Paperback
Страницы: 272
Вес: 0.48 кг.
Дата издания: 02.01.2014
Серия: Cambridge aerospace series
Язык: English
Издание: 2 revised edition
Иллюстрации: Worked examples or exercises; 19 tables, unspecified; 121 line drawings, unspecified
Размер: 179 x 253 x 11
Читательская аудитория: Tertiary education (us: college)
Ключевые слова: Aerospace & aviation technology, TECHNOLOGY & ENGINEERING / Engineering (General)
Основная тема: Engineering
Ссылка на Издательство: Link
Рейтинг:
Поставляется из: Англии
Описание: This text introduces structural dynamics and aeroelasticity, emphasizing conventional aircraft. It considers structural dynamics, static aeroelasticity and dynamic aeroelasticity. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter and elastic tailoring. More than fifty problems enhance student learning.


Principles Of Aeroelasticity

Автор: Bhat
Название: Principles Of Aeroelasticity
ISBN: 1498724728 ISBN-13(EAN): 9781498724722
Издательство: Taylor&Francis
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Цена: 12554.00 р.
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Описание:

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
Introduction to Aircraft Aeroelasticity and Loads

Автор: Wright Jan Robert, Cooper Jonathan E.
Название: Introduction to Aircraft Aeroelasticity and Loads
ISBN: 1118488016 ISBN-13(EAN): 9781118488010
Издательство: Wiley
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Цена: 13931.00 р.
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Описание: Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads.


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