Mineola, New York, Dover Publications, Inc., 2011. 576 p. — ISBN13: 978-0-486-48580-5 (pbk.), ISBN10: 0-486-48580-3 (pbk.)
Still relevant decades after its initial publication, this legendary reference text on aircraft stress analysis is considered the best book on the subject. It emphasizes basic structural theory, which remains unchanged with the development of new materials and construction methods, and the application of elementary principles of mechanics to analysis of aircraft structures. 1950 edition.
Equlibrium of Forces
Space Structures
Inertia Forces and Load Factors
Moments of Inertia, Mohr's Circle
Shear and Bending-Moment Diagrams
Shear and bending Stresses in Symmetrical Beamsd
Beams with Unsymmetrical Cross Sections
Analysis of Typical Members of Semimonocoque Structures
Spanwise Air-Load Distribution.
External Loads om the Airplane
Mechanical Properties of Aircraft Materials
Joints and Fittings
Design of Members in Tension, Bending, or Torison
Design of Compression Members
Design of Webs in Shear
Deflections of Structures
Statistically Indertiminate Structures
Special Methods of Analysis
Appendix