Structural Design Manual Vol 2: A Comprehensive Guide for Aerospace Engineers
The Structural Design Manual Vol 2 is a document that provides detailed information and guidance on the design and analysis of various structural components and systems for aerospace applications. It was published by McDonnell Douglas Corporation, a major American aerospace manufacturer and defense contractor, in 1989.
The manual covers topics such as frames, plates, shear webs, column buckling, plate buckling, stiffness, composite structure, sandwich structure, and transparencies. It also includes examples, tables, charts, graphs, formulas, and references to help engineers perform structural design calculations and evaluations. The manual is intended to supplement the basic principles and methods of structural mechanics and to reflect the current state-of-the-art in structural design practices.
The manual is divided into two volumes: Volume 1 covers the introduction and general aspects of structural design, while Volume 2 focuses on specific structural elements and configurations. The manual is based on the experience and knowledge of McDonnell Douglas engineers who have worked on various aerospace programs such as the F-15 Eagle, the F/A-18 Hornet, the C-17 Globemaster III, the DC-10/MD-11, and the Space Shuttle.
The Structural Design Manual Vol 2 is a valuable resource for aerospace engineers who want to learn more about the theory and application of structural design for aircraft, spacecraft, missiles, rockets, satellites, and other aerospace vehicles. It is also a useful reference for students, researchers, instructors, and professionals who are interested in the field of structural engineering.
One of the main topics covered in the Structural Design Manual Vol 2 is frames. Frames are structural elements that consist of beams and columns joined together to form a rigid structure. Frames are used to support loads and transmit forces and moments to the foundation or other structural components. Frames can be classified into different types based on their geometry, loading, and boundary conditions.
The manual provides detailed information on how to design and analyze frames for various aerospace applications. It covers topics such as frame classification, frame stability, frame buckling, frame deflection, frame vibration, frame optimization, and frame testing. It also presents examples of frame design for aircraft fuselage, wing box, landing gear, engine mount, and space station modules.
Another topic covered in the Structural Design Manual Vol 2 is plates. Plates are structural elements that have a large surface area and a small thickness. Plates are used to form the skin or the outer surface of aerospace vehicles. Plates are subjected to various types of loads such as pressure, shear, bending, torsion, and thermal. Plates can also experience different types of failure modes such as yielding, buckling, cracking, fatigue, and creep.
The manual provides detailed information on how to design and analyze plates for various aerospace applications. It covers topics such as plate theory, plate equations, plate boundary conditions, plate solutions, plate buckling, plate vibration, plate stress analysis, plate fracture mechanics, plate fatigue analysis, and plate thermal analysis. It also presents examples of plate design for aircraft wing, tail, fuselage, nacelle, and control surface. aa16f39245