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

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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 : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-02-14T22:16:46Z No. of bitstreams: 1 FPL_1559-Eocr.pdf: 1973950 bytes, checksum: 78507a7bde2107ca94be8616f4f961e8 (MD5)
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