Other Scholarly Content

 

Stresses within a rectangular, flat sandwich panel subjected to a uniformly distributed normal load and edgewise, direct, and shear loads Public Deposited

Downloadable Content

Download PDF
https://ir.library.oregonstate.edu/concern/defaults/w3763b51q

This report is one of a series issued in cooperation with the Army-Navy-Civil Committee on aircraft design criteria under the supervision of the Aeronautical Board.

Descriptions

Attribute NameValues
Creator
Resource Type
Date Available
Date Issued
Series
Subject
Rights Statement
Publisher
Language
File Format
File Extent
  • 2982515 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
Additional Information
  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-04-20T17:20:14Z No. of bitstreams: 1 FPL_1838ocr.pdf: 2982515 bytes, checksum: 3e298a7b33db48cffb572a83d2d5d36f (MD5)
  • description.provenance : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-06-12T22:12:32Z (GMT) No. of bitstreams: 1 FPL_1838ocr.pdf: 2982515 bytes, checksum: 3e298a7b33db48cffb572a83d2d5d36f (MD5)
  • description.provenance : Made available in DSpace on 2006-06-12T22:12:33Z (GMT). No. of bitstreams: 1 FPL_1838ocr.pdf: 2982515 bytes, checksum: 3e298a7b33db48cffb572a83d2d5d36f (MD5) Previous issue date: 1953-01

Relationships

Parents:

This work has no parents.

Items