Standard Methods for Aerospace Stress Analysis

Standard Methods for Aerospace Stress Analysis

Create safer, more reliable planes with this crucial guide

Aerospace Stress Analysis is the field of research and engineering that evaluates stresses and strains on aerospace structures. By analyzing how different materials and components respond to forces, it helps aerospace engineers build for structural integrity and safety. Combining mathematical and computational models with experimental techniques, it’s a crucial component of developing viable aerospace technologies.

Standard Methods for Aerospace Stress Analysis offers a thorough, practical overview of the structural and stress analysis of both principal and secondary aircraft structures. It covers both fundamental concepts and advanced computational methods, along with key applications. With coverage of both interior and exterior structures, it’s a one-stop shop for all major aspects of stress analysis.

Standard Methods for Aerospace Stress Analysis features:

• Step-by-step examples for every aircraft section
• Detailed discussion of methods including Finite Element Analysis
• An overview of key information on static, fatigue, damage tolerance, buckling, and more

Standard Methods for Aerospace Stress Analysis is ideal for professional mechanical and aerospace engineers working in the aircraft or space industries, as well as students in the field.

Amir Javidinejad received his Ph.D. in Mechanical Engineering from the University of Texas at Arlington, his M.S. in Engineering Mechanics from Georgia Institute of Technology, his B.S. in Mechanical Engineering from the University of Cincinnati, and holds a Certificate in Leadership Mastery from the UCLA-Extension. He has extensive experience in structural/solid mechanics, Finite Element Methods, machine design, and various other stress analysis methods from aerospace, military, and commercial industries, as well as from academia. His expertise and knowledge include space structures analysis, micro sensors analysis, rocket design analysis, helicopter structural repair analysis, airplane structures modifications, aircraft interior monument structures analysis, and certification and qualification testing. He has also been involved in research in the areas of structural mechanics of isotropic, anisotropic, and composite materials. Dr. Javidinejad is a Licensed Professional Mechanical Engineer in the State of California, License #38567, and in the State of Texas, License #141561. Dr. Javidinejad is a member of the Pi Tau Sigma mechanical engineering honor society, a member of the American Society of Mechanical Engineers (ASME), and a member of the American Society of Engineering Education (ASEE). Also, Dr. Javidinejad is currently a part-time Lecturer of Mechanical Engineering in the California State Polytechnic University, Pomona.