Spanwise distribution of aerodynamic shear and bending-moment on cantilever tapered wings
Authors
Hiroshi Sato
The City College of the City University of New York
Keywords:
Aerodynamics, Structures, Design
Abstract
The spanwise air-load distribution for wings with twist is obtained by Schrenk's approximation method..... The shear and bending-moment diagrams are prepared for use in the structural design of sailplane wings.
Author Biography
Hiroshi Sato, The City College of the City University of New York
