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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.
The late David J. Peery was an Aeronautical Engineering Professor at Penn State University.
Preface1. Equlibrium of Forces2. Space Structures3. Inertia Forces and Load Factors4. Moments of Inertia, Mohr's Circle5. Shear and Bending-Moment Diagrams6. Shear and bending Stresses in Symmetrical Beamsd7. Beams with Unsymmetrical Cross Sections8. Analysis of Typical Members of Semimonocoque Structures9. Spanwise Air-Load Distribution. 10. External Loads om the Airplane11. Mechanical Properties of Aircraft Materials12. Joints and Fittings13. Design of Members in Tension, Bending, or Torison14. Design of Compression Members15. Design of Webs in Shear16. Deflections of Structures17. Statistically Indertiminate Structures18. Special Methods of AnalysisAppendixIndex