Finite Element Analysis of Rotating Beams Finite Element Analysis of Rotating Beams
Foundations of Engineering Mechanics

Finite Element Analysis of Rotating Beams

Physics Based Interpolation

    • ‏84٫99 US$
    • ‏84٫99 US$

وصف الناشر

This book addresses the solution of rotating beam free-vibration problems using the finite element method. It provides an introduction to the governing equation of a rotating beam, before outlining the solution procedures using Rayleigh-Ritz, Galerkin and finite element methods. The possibility of improving the convergence of finite element methods through a judicious selection of interpolation functions, which are closer to the problem physics, is also addressed. The book offers a valuable guide for students and researchers working on rotating beam problems – important engineering structures used in helicopter rotors, wind turbines, gas turbines, steam turbines and propellers – and their applications. It can also be used as a textbook for specialized graduate and professional courses on advanced applications of finite element analysis.

النوع
تخصصات مهنية وتقنية
تاريخ النشر
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٨ أغسطس
اللغة
EN
الإنجليزية
عدد الصفحات
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الناشر
Springer Nature Singapore
البائع
Springer Nature B.V.
الحجم
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‫م.ب.‬
Multifidelity Modeling in Vibration Analysis Multifidelity Modeling in Vibration Analysis
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Isospectral Vibrating Systems Isospectral Vibrating Systems
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Structural Health Monitoring Structural Health Monitoring
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The Rotating Beam Problem in Helicopter Dynamics The Rotating Beam Problem in Helicopter Dynamics
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Smart Helicopter Rotors Smart Helicopter Rotors
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Structural Health Monitoring Using Genetic Fuzzy Systems Structural Health Monitoring Using Genetic Fuzzy Systems
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Thermal Engineering Thermal Engineering
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Fundamentals of Tank and Process Equipment Design Fundamentals of Tank and Process Equipment Design
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Acoustic Emission Acoustic Emission
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Rational and Applied Mechanics Rational and Applied Mechanics
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Mechanical Vibrations Mechanical Vibrations
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The Rotating Beam Problem in Helicopter Dynamics The Rotating Beam Problem in Helicopter Dynamics
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