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Rationalization in Deriving Element Stiffness Matrix by Assumed Stress Approach
Author(s): Pian, Theodore H. H., Tong, Pin
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 441-469
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A Finite Element Application of the Hellinger-Reissner Variational Theorem
Author(s): Dunham, Robert S., Pister, Karl S.
Corporate Author(s): University of California, Berkeley
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 471-487
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Finite Elements in Linear Viscoelasticity
Author(s): White, J. L.
Corporate Author(s): Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 489-516
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Finite Element Analysis of Fluid Flows
Author(s): Martin, Harold C.
Corporate Author(s): Univeristy of Washnigton
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 517-535
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Curved Thick Shell and Membrane Elements with Particular Reference to Axisymmetric Problems
Author(s): Ahmad, Sohrabuddin, Irons, Bruce M.
Corporate Author(s): Technological University
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 539-572
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Finite Element Analysis of Sandwich Plates and Cylindrical Shells with Laminated Faces
Author(s): Monforton, G. R., Schmit, L. A., Jr.
Corporate Author(s): Case Western Reserve University
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 573-616
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Curved Triangular Elements for the Analysis of Shells
Author(s): Bonnes, G., Giroux, Y. M., Robichaud, L. P. A., Dhatt, G.
Corporate Author(s): Laval University
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 617-639
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A Doubly Curved Triangular Shell Element
Author(s): Strickland, Gordon E., Jr., Loden, William A.
Corporate Author(s): Lockheed Missiles and Space Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 641-666
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The Analysis of Thin Shells with Transverse Shear Strains by the Finite Element Method
Author(s): Key, Samuel W., Beisinger, Zelma E.
Corporate Author(s): Sandia Laboratories
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 667-710
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Elastic Instability Predictions for Doubly-Curved Shells
Author(s): Gallagher, Richard H., Yang, Henry T. Y.
Corporate Author(s): Cornell University
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 711-739

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