02040nam 2200445 450 991070528910332120141222112304.0(CKB)5470000002448472(OCoLC)898480937(EXLCZ)99547000000244847220141222d1962 ua 0engurbn|||||||||rdacontentrdamediardacarrierFatigue of sandwich constructions for aircraft, cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear /by Fred WerrenMadison, Wisconsin :United States Department of Agriculture, Forest Service, Forest Products Laboratory,1962.1 online resource (8 unnumbered pages) illustrationsReport ;no. 1559-ETitle from title screen (viewed Dec. 17, 2014)."Information reviewed and reaffirmed 1962."Publication pre-dates Federal Depository Library Program (FDLP) item numbers. No FDLP item number has been assigned"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.""In cooperation with the University of Wisconsin."Includes bibliographical references.Cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shearSandwich constructionAluminumSandwich construction.Aluminum.Werren Fred1385908Forest Products Laboratory (U.S.),University of Wisconsin.GPOGPOBOOK9910705289103321Fatigue of sandwich constructions for aircraft, cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear3465919UNINA