Über den Autor
G. Lakshmi NarasaiahMechanical engineering graduate from NIT (formerly REC), WarangalM.Tech (Aero) from IIT, KanpurWorked in BHEL for 25 years, undertaking FEA for many new designs with extensive applications using software SAP-IV, STRUDL, PAFEC & ANSYSDeveloped post-processors for solutions from FEA software for fatigue & creep analysis leading to Residual Life Assessment of thermal power plant components.Developed routines for validation of results as per ASME B&PV code, section IIITaught Finite Element Method and Engineering Mechanics in addition to other design subjects to engineering students, affiliated to JNTU, Hyderabad, JNTU, Kakinada and Osmania University for about 10 yearsTaught Aircraft Structures to students of Institute of Aeronautical Engineering, MLR Institute of Technology, MNR college of Engineering (affiliated to JNTU, Hyderabad)Authored books on 'Engineering Mechanics' and 'Finite Element Analysis' which are essential for the design and analysis of Aircraft Structures
Klappentext
Aircraft structures, with emphasis on light weight, 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. These are also susceptible to buckling, aeroelastic deformation and fatigue.nThis book covers comprehensive reading material for the students of Aerospace engineering and caters to the subject usually covered in two semesters.nSpecial Features:All related topics, such as engineering mechanics, strength of materials, theory of elasticity and Aerodynamics are briefly coverednSolved problems provided; additional problems included for practice by studentsnTopics like Fatigue analysis, FEM, Aeroelasticity and materials are includednBased on the feedback received for the 1st edition, some associated topics were briefly covered
