Compressive and Tensile Creep of 7075-T6 and 2024-T3 Aluminum-alloy Sheet
Author : George J. Heimerl
Publisher :
Page : 48 pages
File Size : 44,31 MB
Release : 1959
Category : Materials
ISBN :
Author : George J. Heimerl
Publisher :
Page : 48 pages
File Size : 44,31 MB
Release : 1959
Category : Materials
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 448 pages
File Size : 30,47 MB
Release : 1960
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 860 pages
File Size : 22,61 MB
Release : 1957
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 878 pages
File Size : 31,50 MB
Release : 1961
Category : Aeronautics
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : pages
File Size : 40,85 MB
Release : 1960-07
Category :
ISBN :
Author :
Publisher :
Page : 494 pages
File Size : 12,70 MB
Release : 1959
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 818 pages
File Size : 38,75 MB
Release : 1954
Category : Aeronautics
ISBN :
Author : Josef Singer
Publisher : John Wiley & Sons
Page : 1140 pages
File Size : 20,57 MB
Release : 2002-08-12
Category : Technology & Engineering
ISBN : 0471974501
* Edited by Josef Singer, the world's foremost authority on structural buckling. * Time-saving and cost-effective design data for all structural, mechanical, and aerospace engineering researchers.
Author : Ilan Mosche Levi
Publisher :
Page : 188 pages
File Size : 41,6 MB
Release : 1968
Category : Buckling (Mechanics)
ISBN :
The effect of creep on the load carrying ability of plates was investigated. The plates were loaded by compressive forces applied in the plane of the plate. It was assumed that the material deforms due to linear elasticity and steady state creep, and creep strain rate is given by the power law. When a fixed uniaxial load is applied to the plate in such a way that the load remains uniformly distributed during the buckling process, the governing equations indicate that a finite time exists after which the lateral deformations of the plate become unbounded. Simple, closed form expressions for this critical time are derived for various values of the creep exponent, and for the case where primary creep plays an important role. (Author).
Author : United States. National Bureau of Standards
Publisher :
Page : 1114 pages
File Size : 13,76 MB
Release : 1966
Category : Engineering
ISBN :