Aircraft Structures
Autor G. Lakshmi Narasaiahen Limba Engleză Hardback – 12 iul 2011
The first part deals with the basics of structural analysis, including mechanics or rigid bodies, energy principles, analysis of trusses, and analysis of continuum structures. In the second part, basic aerodynamics, loads, beams, shafts, buckling of columns, bending and buckling of thin plates and shear flow, shear center and shear lag, aeroplane fuselage and wing and fatigue are explained. The third section covers additional topics, such as finite element analysis, aircraft construction materials and aeroelasticity. With an emphasis on lightweight design, this volume further presents some special topics, such as box beams in wings, ring frames in fuselage, and longitudinal stiffeners.
With many examples and solved problems, this textbook on aircraft structures is an essential source of information for both students and engineering professionals who want to introduce themselves to the topic.
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Specificații
ISBN-13: 9780415665742
ISBN-10: 0415665744
Pagini: 430
Dimensiuni: 182 x 247 x 23 mm
Greutate: 0.91 kg
Ediția:New.
Editura: The Book Syndicate
Colecția CRC Press
ISBN-10: 0415665744
Pagini: 430
Dimensiuni: 182 x 247 x 23 mm
Greutate: 0.91 kg
Ediția:New.
Editura: The Book Syndicate
Colecția CRC Press
Public țintă
Professional Practice & Development and UndergraduateCuprins
Introduction Part 1. Basics of Structural Analysis Part 2. Design and Analysis of Aeroplane Structures Part 3. Other Relevant Topics
Notă biografică
G Lakshmi Narasaiah is a professor at the Institute of Aeronautical Engineering, affiliated to the Jawarhalal Nehru University of Technology, Hyderabad, India, where he works on engineering mechanics, machine design and finite element analysis. Educated as a mechanical engineer and specialized in Aero-structures, he worked for over 25 years at Bharat Heavy Electrical Ltd and gained both broad and deep knowledge and expertise of finite element analysis of power plant structure and pressure vessels.
Descriere
This textbook addresses topics associated with aircraft structures, such as engineering mechanics, strength of materials, theory of elasticity, and aerodynamics. With an emphasis on light weight, aircraft structures have incorporated special features such as box beams in wings, ring frames in fuselage, and longitudinal stiffeners. These are designed for bending, shear and torsion loads, and they are also susceptible to buckling, aeroelastic deformation, and fatigue. Providing additional study material, this book offers comprehensive coverage for students of aerospace engineering.