LEADER 02040nam  2200445   450 
001 9910705289103321
005 20141222112304.0
035   $a(CKB)5470000002448472
035   $a(OCoLC)898480937
035   $a(EXLCZ)995470000002448472
100   $a20141222d1962      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $2rdacontent
182   $2rdamedia
183   $2rdacarrier
200 10$aFatigue of sandwich constructions for aircraft, cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear /$fby Fred Werren
210  1$aMadison, Wisconsin :$cUnited States Department of Agriculture, Forest Service, Forest Products Laboratory,$d1962.
215   $a1 online resource (8 unnumbered pages) $cillustrations
225 1 $aReport ;$vno. 1559-E
300   $aTitle from title screen (viewed Dec. 17, 2014).
300   $a"Information reviewed and reaffirmed 1962."
300   $aPublication pre-dates Federal Depository Library Program (FDLP) item numbers. No FDLP item number has been assigned
300   $a"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."
300   $a"In cooperation with the University of Wisconsin."
320   $aIncludes bibliographical references.
517 3 $aCellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear
606   $aSandwich construction
606   $aAluminum
615  0$aSandwich construction.
615  0$aAluminum.
700   $aWerren$b Fred$01385908
712 02$aForest Products Laboratory (U.S.),
712 02$aUniversity of Wisconsin.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705289103321
996   $aFatigue of sandwich constructions for aircraft, cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear$93465919
997   $aUNINA