Контакты/Проезд  Доставка и Оплата Помощь/Возврат
История
  +7(495) 980-12-10
  пн-пт: 10-18 сб,вс: 11-18
  shop@logobook.ru
   
    Поиск книг                    Поиск по списку ISBN Расширенный поиск    
Найти
  Зарубежные издательства Российские издательства  
Авторы | Каталог книг | Издательства | Новинки | Учебная литература | Акции | Хиты | |
 

Aeroelastic vibrations and stability of plates and shells, Sergey D. Algazin,Igor A. Kijko


Варианты приобретения
Цена: 33463.00р.
Кол-во:
Наличие: Поставка под заказ.  Есть в наличии на складе поставщика.
Склад Америка: Есть  
При оформлении заказа до:
Ориентировочная дата поставки:
При условии наличия книги у поставщика.

Добавить в корзину
в Мои желания

Автор: Sergey D. Algazin,Igor A. Kijko
Название:  Aeroelastic vibrations and stability of plates and shells
ISBN: 9783110338362
Издательство: Walter de Gruyter
Классификация:






ISBN-10: 311033836X
Обложка/Формат: Hardback
Страницы: 231
Вес: 0.48 кг.
Дата издания: 17.11.2014
Серия: Physics
Язык: English
Размер: 241 x 173 x 20
Читательская аудитория: Professional and scholarly
Ключевые слова: Classical mechanics,Mathematical physics,Mechanical engineering,Automotive (motor mechanic) skills, SCIENCE / Mechanics / Aerodynamics,SCIENCE / Physics / Mathematical & Computational,TECHNOLOGY & ENGINEERING / Automotive
Поставляется из: Германии
Описание: Back-action of aerodynamics onto structures such as wings cause vibrations and may resonantly couple to them, thus causing instabilities (flutter) and endangering the whole structure. By careful choices of geometry, materials and damping mechanisms, hazardous effects on wind engines, planes, turbines and cars can be avoided. Besides an introduction into the problem of flutter, new formulations of flutter problems are given as well as a treatise of supersonic flutter and of a whole range of mechanical effects. Numerical and analytical methods to study them are developed and applied to the analysis of new classes of flutter problems for plates and shallow shells of arbitrary plane form. Specific problems discussed in the book in the context of numerical simulations are supplemented by Fortran code examples (available on the website).


Nonlinear Vibrations and Stability of Shells and Plates

Автор: Amabili
Название: Nonlinear Vibrations and Stability of Shells and Plates
ISBN: 1107435420 ISBN-13(EAN): 9781107435421
Издательство: Cambridge Academ
Рейтинг:
Цена: 10138.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: This book covers theoretical and experimental aspects of nonlinear vibrations and stability of shells and plates including recent progresses in nonlinear vibrations and stability, advanced problems of shells with fluid-structure interaction, and many practical concepts, diagrams, and numerical results.

Vibrations and Waves

Автор: King George
Название: Vibrations and Waves
ISBN: 0470011890 ISBN-13(EAN): 9780470011898
Издательство: Wiley
Рейтинг:
Цена: 6645.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: Emphasizes the physical principles, placing the physics before the mathematics. Each chapter includes problems ranging in difficulty from simple to challenging. Includes hints for solving problems. Numerous worked examples included throughout the book. More advanced material is included in optional sections marked with an asterisk. .

Principles Of Aeroelasticity

Автор: Bhat
Название: Principles Of Aeroelasticity
ISBN: 1498724728 ISBN-13(EAN): 9781498724722
Издательство: Taylor&Francis
Рейтинг:
Цена: 12554.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

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
Рейтинг:
Цена: 13931.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

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.

Introduction to Structural Dynamics and Aeroelasticity

Автор: Hodges
Название: Introduction to Structural Dynamics and Aeroelasticity
ISBN: 110761709X ISBN-13(EAN): 9781107617094
Издательство: Cambridge Academ
Рейтинг:
Цена: 8395.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

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.


ООО "Логосфера " Тел:+7(495) 980-12-10 www.logobook.ru
   В Контакте     В Контакте Мед  Мобильная версия