Other Scholarly Content
 

Design curves for the buckling of sandwich cylinders of finite length under uniform external lateral pressure

Public Deposited

Downloadable Content

Download PDF
https://ir.library.oregonstate.edu/concern/defaults/br86b756j

Descriptions

Attribute NameValues
Creator
Abstract
  • This report is one of a series issued in cooperation with the ANC-23 Panel on Composite Construction for Flight Vehicles of the Departments of the Air Force, Navy, and Commerce
Resource Type
Date Available
Date Issued
Series
Subject
Rights Statement
Publisher
Language
File Format
File Extent
  • 1674106 bytes
Digitization Specifications
  • Scanned at 600 DPI using a Cannon DR-9080C in TIF format. PDF generated through Capture Perfect using OmniPage 14 Pro for textual OCR.
Replaces

Relationships

Parents:

This work has no parents.

Items