Other Scholarly Content

 

Fatigue of sandwich constructions for aircraft : Aluminum face and paper honeycomb core sandwich material tested in shear Public Deposited

Downloadable Content

Download PDF
https://ir.library.oregonstate.edu/concern/defaults/qn59q731v

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
  • 3618593 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 : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-04-14T15:54:54Z (GMT) No. of bitstreams: 1 FPL_1559-Aocr.pdf: 3618593 bytes, checksum: f850b49b7b13fcf7cc82f9318bb5949b (MD5)
  • description.provenance : Made available in DSpace on 2006-04-14T15:54:55Z (GMT). No. of bitstreams: 1 FPL_1559-Aocr.pdf: 3618593 bytes, checksum: f850b49b7b13fcf7cc82f9318bb5949b (MD5) Previous issue date: 1947-12
  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-04-12T17:54:06Z No. of bitstreams: 1 FPL_1559-Aocr.pdf: 3618593 bytes, checksum: f850b49b7b13fcf7cc82f9318bb5949b (MD5)

Relationships

Parents:

This work has no parents.

Items