Creep bending and buckling of thin circular cylindrical shells - Erickson, Burton; Polytechnic Institute of Brooklyn (Washington, [D.C.] : National Aeronautics and Space Administration, 1960)
"NASA TN D-429."
"Polytechnic Institute of Brooklyn."
"June 1960."
Cover title.
Includes bibliographical references (p. 28).
Also 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.
Keywords: Temperature effects; Load tests; Cylindrical shells; Circular shells; Aluminum alloys; Aerodynamic loads; Thin walled shells; Elastoplasticity; Deformation; Creep buckling; Creep analysis; Bending