Fatigue of sandwich constructions for aircraft : Aluminum face and end-grain balsa core sandwich material tested in shear Public Deposited

http://ir.library.oregonstate.edu/concern/defaults/8c97kv15n

Information reviewed and reaffirmed March 1956 and 1962

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  • description.provenance : Made available in DSpace on 2006-04-17T19:06:49Z (GMT). No. of bitstreams: 1 FPL_1559-Bocr.pdf: 2203640 bytes, checksum: 3379d84e1278b8d31ef2536092e44bef (MD5) Previous issue date: 1962
  • description.provenance : Approved for entry into archive by Terry Reese Jr(terry.reese@oregonstate.edu) on 2006-04-17T19:06:48Z (GMT) No. of bitstreams: 1 FPL_1559-Bocr.pdf: 2203640 bytes, checksum: 3379d84e1278b8d31ef2536092e44bef (MD5)
  • description.provenance : Submitted by Adam Powell (powella@onid.orst.edu) on 2006-04-12T17:47:54Z No. of bitstreams: 1 FPL_1559-Bocr.pdf: 2203640 bytes, checksum: 3379d84e1278b8d31ef2536092e44bef (MD5)

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