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.

Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 4. Application of the Electric Analog Computer to the Elastic Plate Problem

Report Number: AF TR 5761 Part 4
Author(s): Richard H. MacNeal
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 1950-10-01
Pages: 119
Contract: W33-038-ac-16961
Contract: 462-50
AD Number: AD0089754

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

This citation is provided as a resource for researchers, but Contrails cannot provide a full-image download

U.S. government employees, Military/Department of Defense employees, and U.S. government contractors and sub-contractors may be eligible to register with the Defense Technical Information Center (DTIC), where this report and others like it may be available

Other options for obtaining this report

Via the Defense Technical Information Center (DTIC):
This report is not publicly available via DTIC

Via National Technical Information Service:
This report is unlikely to be available in 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

Related Reports

This report has the following parts/volumes: