The Investigation of Structural Members Under Combined Axial and Transverse Loads. Section 1. Air Service Information Circular, Volume 5, Number 493.
AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH WRIGHT RESEARCH SITE
Pagination or Media Count:
Historical study that provides a satisfactory method of computing the stresses in such members of an airplace structure as are subjected to combined axial and transverse. The purpose of the investigation was to make a comparative study of a number of approximate methods for the design of members under combined loads to ascertain their relative degrees of conservatism and ease of application.
- Research and Experimental Aircraft
- Laminates and Composite Materials