Accurate calculation of multispar cantilever and semicantilever wings with parallel webs under direct and indirect loading
Description: In the present report the computation is actually carried through for the case of parallel spars of equal resistance in bending without direct loading, including plotting of the influence lines; for other cases the method of calculation is explained. The development of large size airplanes can be speeded up by accurate methods of calculation such as this.
Date: March 1932
Creator: Sanger, Eugen
Item Type: Report
Partner: UNT Libraries Government Documents Department