Torsional stiffness of thin-walled shells having reinforcing cores and rectangular, triangular, or diamond cross section
A theoretical investigation is presented of the torsional stiffness of thin-walled aerodynamic surfaces filled with cores which stabilize the skins. Rectangular, slender triangular, and slender diamond cross sections are considered. Results for the torsional stiffness constants are shown graphically.
BEAMS, STRUCTURAL↗