Fatigue of sandwich constructions for aircraft : Cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear Public Deposited

http://ir.library.oregonstate.edu/concern/defaults/44558j33v

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on aircraft design criteria under the supervision of the Aircraft Committee of the Munitions Board. Information reviewed and reaffirmed 1956 and 1962. Original report issued October 1948.

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  • description.provenance : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-04-11T16:35:45Z (GMT) No. of bitstreams: 1 FPL_1559-Eocr.pdf: 1973950 bytes, checksum: 78507a7bde2107ca94be8616f4f961e8 (MD5)
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