LEADER 02021nam  2200457   450 
001 9910705289003321
005 20141222112759.0
035   $a(CKB)5470000002448473
035   $a(OCoLC)898481010
035   $a(EXLCZ)995470000002448473
100   $a20141222d1948      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $2rdacontent
182   $2rdamedia
183   $2rdacarrier
200 10$aFatigue of sandwich constructions for aircraft, cellular cellulose acetate core material with aluminum or fiberglas-laminate facings, tested in shear /$fby Fred Werren
210  1$aMadison, Wisconsin :$cUnited States Department of Agriculture, Forest Service, Forest Products Laboratory,$d1948.
215   $a1 online resource (11 unnumbered pages) $cillustrations
225 1 $aReport ;$vno. 1559-F
300   $aTitle from title screen (viewed Dec. 17, 2014).
300   $a"December 1948."
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.
606   $aSandwich construction
606   $aCore materials$xTesting
606   $aStrength of materials
615  0$aSandwich construction.
615  0$aCore materials$xTesting.
615  0$aStrength of materials.
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   $a9910705289003321
996   $aFatigue of sandwich constructions for aircraft, cellular cellulose acetate core material with aluminum or fiberglas-laminate facings, tested in shear$93532563
997   $aUNINA