Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials PanelPublisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 600
Book Description
Manual on Aeroelasticity: Prediction of aeroelastic phenomena
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials PanelPublisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 374
Book Description
Manual on Aeroelasticity
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials PanelPublisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 196
Book Description
Manual on Aeroelasticity
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Structures and Materials PanelPublisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 338
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 602
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
AGARD Index of Publications
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and DevelopmentPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 410
Book Description
AGARD Index of Publications
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Technical Information PanelPublisher:
ISBN:
Category :
Languages : en
Pages : 206
Book Description
Index to AGARD Publications
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and DevelopmentPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 336
Book Description
Index Aeronauticus
Author: Introduction to Aircraft Aeroelasticity and Loads
Author: Jan Robert WrightPublisher: John Wiley & Sons
ISBN: 0470858400
Category : Technology & Engineering
Languages : en
Pages : 527
Book Description
Aircraft performance is influenced significantly both by aeroelastic phenomena, arising from the interaction of elastic, inertial and aerodynamic forces, and by load variations resulting from flight and ground manoeuvres and gust / turbulence encounters. There is a strong link between aeroelasticity and loads, and these topics have become increasingly integrated in recent years. Introduction to Aircraft Aeroelasticity and Loads introduces the reader to the main principles involved in a wide range of aeroelasticity and loads topics. Divided into three sections, the book begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control. It goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response before introducing more advanced methodologies. Finally, it explains how industrial certification requirements for aeroelasticity and loads may be met and relates these to the earlier theoretical approaches used. Presents fundamentals of structural dynamics, aerodynamics, static and dynamic aeroelasticity, response and load calculations and testing techniques. Covers performance issues related to aeroelasticity such as flutter, control effectiveness, divergence and redistribution of lift. Includes up-to-date experimental methods and analysis. Accompanied by a website with MatLAB and SIMULINK programs that relate to the models used. Introduction to Aircraft Aeroelasticity and Loads enables the reader to understand the aeroelastic and loads principles and procedures employed in a modern aircraft design office. It will appeal to final year undergraduate and masters students as well as engineers who are new to the aerospace industry.
Introduction to Aircraft Aeroelasticity and Loads
Author: Jan R. WrightPublisher: John Wiley & Sons
ISBN: 1118488016
Category : Technology & Engineering
Languages : en
Pages : 580
Book Description
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. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response and loads for the flexible aircraft before introducing some more advanced methodologies. Finally, it explains how industrial certification requirements for aeroelasticity and loads may be met and relates these to the earlier theoretical approaches used. Key features of this new edition include: Uses a unified simple aeroelastic model throughout the book Major revisions to chapters on aeroelasticity Updates and reorganisation of chapters involving Finite Elements Some reorganisation of loads material Updates on certification requirements Accompanied by a website containing a solutions manual, and MATLAB® and SIMULINK® programs that relate to the models used Introduction to Aircraft Aeroelasticity and Loads, Second Edition is a must-have reference for researchers and practitioners working in the aeroelasticity and loads fields, and is also an excellent textbook for senior undergraduate and graduate students in aerospace engineering.