01778nam 2200421 450 991070528930332120141223161656.0(CKB)5470000002448470(OCoLC)898616541(EXLCZ)99547000000244847020141223d1956 ua 0engurbn|||||||||rdacontentrdamediardacarrierFatigue of sandwich constructions for aircraft, fiberglas-honeycomb core material with fiberglas-laminate or aluminum facings, tested in shear /by Fred WerrenMadison, Wisconsin :United States Department of Agriculture, Forest Service, Forest Products Laboratory,1956.1 online resource (10 unnumbered pages) illustrationsReport ;no. 1559-CTitle from title screen (viewed Dec. 23, 2014)."Information reviewed and reaffirmed March 1956."Publication pre-dates Federal Depository Library Program (FDLP) item numbers. No FDLP item number has been assigned."In cooperation with the University of Wisconsin."Fiberglas-honeycomb core material with fiberglas-laminate or aluminum facings, tested in shearSandwich constructionAluminumSandwich construction.Aluminum.Werren Fred1385908Forest Products Laboratory (U.S.),University of Wisconsin.GPOGPOBOOK9910705289303321Fatigue of sandwich constructions for aircraft, fiberglas-honeycomb core material with fiberglas-laminate or aluminum facings, tested in shear3477387UNINA