Flat sheet metal girder with very thin metal web : Part 2 : Sheet metal girders with spars resistant to bending - oblique uprights - stiffness /

Bibliographic Details
Main Author: Wagner, Herbert, 1900-1982
Corporate Authors: Knovel (Firm), United States. National Advisory Committee for Aeronautics
Format: eBook
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1931]
Series:Technical memorandums (United States. National Committee for Aeronautics) ; no. 605.
Subjects:
Online Access:Connect to the full text of this electronic book
Description
Abstract:Noting that the stiffness of the girder increases very rapidly as Beta increases, the result can be summed up as follows: When the cross stress preponderates in one direction and when the web plate is to be given the dimensions commensurate to its stresses, it is advisable (regardless of any ensuing structural difficulties) to set the uprights at about Beta = 120 degrees, thereby lowering the weight of the plate wall 15 percent (in contrast to Beta = 90 degrees), and raising the stiffness 55 percent. But, when the cross stresses alternate and are approximately of the same intensity in both directions, or, if the web plate thickness is determined by other structural reasons, then Beta = 90 degrees should be chosen.
Item Description:"February, 1931."
NACA TM Number 605.
Translated from Zeitschrift fur Flugtechnik und Motorluftschiffahrt. Volume 20, Number 9, May 14, Number 10, May 28, and Number 11, June 14, 1929, by the National Advisory Committee for Aeronautics.
Electronic resource.
Physical Description:1 online resource (38 pages, 6 unnumbered pages) : illustrations.
ISBN:9781680156591
1680156594