AGARD Manual on Aeroelasticity in Axial-flow Turbomachines: Structural dynamics and aeroelasticity PDF Download
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Author: Max F. Platzer
Publisher:
ISBN: 9789283504672
Category : Aeroelasticity
Languages : en
Pages : 200
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Book Description
The first volume of this Manual reviewed the state of the art of unsteady turbomachinery aerodynamics as required for the study of aeroelasticity in axial turbomachines. This second volume aims to complete the review by presenting the state of the art of structural dynamics and of aeroelasticity. The eleven chapters in this second volume give an overview of the subject and reviews of the structural dynamics characteristics and analysis methods applicable to single blades and bladed assemblies. The blade fatigue problem and its assessment methods, and life-time prediction are considered. Aeroelastic topics covered: the problem of blade-disc shroud aeroelastic coupling, formulations and solutions for tuned and mistuned rotors, and instrumentation on test procedures to perform a fan flutter test. The Effect of stagnation temperature and pressure on flutter is demonstrated and currently available forced vibration and flutter design methodology is reviewed.
Author: Max F. Platzer
Publisher:
ISBN: 9789283504672
Category : Aeroelasticity
Languages : en
Pages : 200
Get Book
Book Description
The first volume of this Manual reviewed the state of the art of unsteady turbomachinery aerodynamics as required for the study of aeroelasticity in axial turbomachines. This second volume aims to complete the review by presenting the state of the art of structural dynamics and of aeroelasticity. The eleven chapters in this second volume give an overview of the subject and reviews of the structural dynamics characteristics and analysis methods applicable to single blades and bladed assemblies. The blade fatigue problem and its assessment methods, and life-time prediction are considered. Aeroelastic topics covered: the problem of blade-disc shroud aeroelastic coupling, formulations and solutions for tuned and mistuned rotors, and instrumentation on test procedures to perform a fan flutter test. The Effect of stagnation temperature and pressure on flutter is demonstrated and currently available forced vibration and flutter design methodology is reviewed.
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials Panel
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 196
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Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials Panel
Publisher:
ISBN:
Category : Transportation
Languages : en
Pages : 506
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Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials Panel
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 170
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Book Description
Author: Max F. Platzer
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: Jan R. Wright
Publisher: John Wiley & Sons
ISBN: 1118488016
Category : Technology & Engineering
Languages : en
Pages : 580
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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.
Author: E. C. Pike
Publisher:
ISBN:
Category :
Languages : en
Pages : 25
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Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Structures and Materials Panel
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 686
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Book Description
