The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

Crack Propogation in Aluminum Alloy Sheet Materials Under Flight-Simulation Loading

Report Number: AFFDL TR 69-50
Author: Schijve, J.
Author: Tromp, P. J.
Author: Jacobs, F. A.
Corporate Author: National Aerospace Laborator, Amsterdam, The Netherlands
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1970-09
Pages: 76
Contract: F61052-67-C-0076
Project: None Given
AD Number: AD0715331

The abstract for this report is either unavailable or has yet to be entered

Lockheed Martin Missiles & Fire Control
Download this report

(PDF, 2.19 MB, 76 pages)

Other options for obtaining this report

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a full-image download of the report, exists at DTIC

Via National Technical Information Service:
The NTIS Order Number for this report is: AD715331
This report may have been digitized and made freely available for public download, or made publicly available for purchase by the National Technical Information Service through their online database, the National Technical Reports Library

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement