Creep bending and buckling of thin circular cylindrical shells

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024	8	⊔	‡a89N70957
024	8	⊔	‡a19890068584
035	⊔	⊔	‡asdr-uiuc6396538
035	⊔	⊔	‡a(OCoLC)73335103
040	⊔	⊔	‡aFER ‡cFER
049	⊔	⊔	‡aUIUU
245	0	0	‡aCreep bending and buckling of thin circular cylindrical shells / ‡cby Burton Erickson ... [et. al].
260	⊔	⊔	‡aWashington, [D.C.] : ‡bNational Aeronautics and Space Administration, ‡c1960.
300	⊔	⊔	‡a49 p. : ‡bill. ; ‡c26 cm.
490	⊔	0	‡aNASA technical note ; ‡vD-429
500	⊔	⊔	‡a"NASA TN D-429."
500	⊔	⊔	‡a"Polytechnic Institute of Brooklyn."
500	⊔	⊔	‡a"June 1960."
500	⊔	⊔	‡aCover title.
504	⊔	⊔	‡aIncludes bibliographical references (p. 28).
530	⊔	⊔	‡aAlso available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 10/16/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068584_1989068584.pdf.
538	⊔	⊔	‡aMode of access: Internet.
650	⊔	7	‡aTemperature effects. ‡2nasat
650	⊔	7	‡aLoad tests. ‡2nasat
650	⊔	7	‡aCylindrical shells. ‡2nasat
650	⊔	7	‡aCircular shells. ‡2nasat
650	⊔	7	‡aAluminum alloys. ‡2nasat
650	⊔	7	‡aAerodynamic loads. ‡2nasat
650	⊔	7	‡aThin walled shells. ‡2nasat
650	⊔	7	‡aElastoplasticity. ‡2nasat
650	⊔	7	‡aDeformation. ‡2nasat
650	⊔	7	‡aCreep buckling. ‡2nasat
650	⊔	7	‡aCreep analysis. ‡2nasat
650	⊔	7	‡aBending. ‡2nasat
700	1	⊔	‡aErickson, Burton.
710	2	⊔	‡aPolytechnic Institute of Brooklyn.
CID	⊔	⊔	‡a011448211
DAT	0	⊔	‡a20101105110132.0 ‡b20141009010000.0
DAT	1	⊔	‡a20141112165512.0 ‡b2024-01-23T18:44:56Z
CAT	⊔	⊔	‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
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