Buckling loads of flat sandwich panels in compression : The buckling of flat sandwich panels with edges simply supported (End grain balsa cores and facings of aluminum and glass cloth laminate) Public Deposited

http://ir.library.oregonstate.edu/concern/defaults/w3763b474

This report is one of a series issued in cooperation withe the Army-Navy-Civil Committee on aircraft design criteria under the supervision of the Aeronautical Board. Information reviewed and reaffirmed Janary 1954 and 1960.

Descriptions

Attribute NameValues
Creator
Resource Type
Date Available
Date Issued
Series
Subject
Rights Statement
Publisher
Language
File Format
File Extent
  • 9244933 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 2006-02-09T18:49:42Z No. of bitstreams: 1 FPL_1525-Aocr.pdf: 9244933 bytes, checksum: 85141e759972c84da9351de96641637e (MD5)
  • description.provenance : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-03-13T16:58:48Z (GMT) No. of bitstreams: 1 FPL_1525-Aocr.pdf: 9244933 bytes, checksum: 85141e759972c84da9351de96641637e (MD5)
  • description.provenance : Made available in DSpace on 2006-03-13T16:58:49Z (GMT). No. of bitstreams: 1 FPL_1525-Aocr.pdf: 9244933 bytes, checksum: 85141e759972c84da9351de96641637e (MD5) Previous issue date: 1960

Relationships

In Administrative Set:
Last modified: 09/22/2017

Downloadable Content

Download PDF
Citations:

EndNote | Zotero | Mendeley

Items