LEADER 02020nam  2200469   450 
001 9910705289703321
005 20141222153016.0
035   $a(CKB)5470000002448466
035   $a(OCoLC)898493911
035   $a(EXLCZ)995470000002448466
100   $a20141222d1947      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $2rdacontent
182   $2rdamedia
183   $2rdacarrier
200 10$aFatigue of sandwich constructions for aircraft, aluminum face and paper honeycomb core sandwich material tested in shear /$fby Fred Werren
210  1$aMadison, Wisconsin :$cUnited States Department of Agriculture, Forest Service, Forest Products Laboratory,$d1947.
215   $a1 online resource (13 unnumbered pages) $cillustrations
225 1 $aReport ;$vno. 1559-A
300   $aTitle from title screen (viewed Dec. 18, 2014).
300   $a"December 1947."
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 Army-Navy-Civil Committee on Aircraft Design Criteria under the supervision of the Aeronautical Board.
300   $a"In cooperation with the University of Wisconsin.
320   $aIncludes bibliographical references.
517 3 $aAluminum face and paper honeycomb core sandwich material tested in shear
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   $a9910705289703321
996   $aFatigue of sandwich constructions for aircraft, aluminum face and paper honeycomb core sandwich material tested in shear$93448994
997   $aUNINA