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    Multiobjective Design of an Antisymmetric Angle-Ply Laminate by Nonlinear Programming 

    Source: Journal of Mechanical Design:;1983:;volume( 105 ):;issue: 002:;page 214
    Author(s): S. Adali
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An antisymmetrically laminated angle-ply plate is optimized with the objectives of minimizing the maximum dynamic deflection, maximizing the natural frequencies and/or maximizing the buckling load. ...
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    Optimization of Antisymmetric Angle-Ply Strip for Maximum Strength Including Hygrothermal Effects 

    Source: Journal of Mechanical Design:;1987:;volume( 109 ):;issue: 003:;page 392
    Author(s): S. Adali; H. Nissen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The transverse failure load on an antisymmetrically laminated angle-ply strip is maximized with respect to fiber volume ratio. The failure load is determined using the Tsai-Hill failure theory ...
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    Optimal Design of Laminated Cylindrical Pressure Vessels for Maximum External Pressure 

    Source: Journal of Pressure Vessel Technology:;1997:;volume( 119 ):;issue: 004:;page 494
    Author(s): M. Walker; S. Adali; T. Reiss
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Finite element solutions are presented for the optimal design of hemispherically and flat-capped symmetrically laminated pressure vessels subjected to external pressure. The effect of vessel length, ...
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    Minimum Weight Design of Symmetric Angle-Ply Laminates With Incomplete Information on Initial Imperfections 

    Source: Journal of Applied Mechanics:;1997:;volume( 064 ):;issue: 001:;page 90
    Author(s): S. Adali; A. Richter; V. E. Verijenko
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An angle-ply laminated plate is optimized with the objective of minimizing its weight subject to maximum deflection and buckling constraints. The plate has an initial deflection the shape of ...
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    Design/Control Optimization of Cross‐Ply Laminates Under Buckling and Vibration 

    Source: Journal of Aerospace Engineering:;1992:;Volume ( 005 ):;issue: 001
    Author(s): J. M. Sloss; I. S. Sadek; J. C. Bruch, Jr.; S. Adali
    Publisher: American Society of Civil Engineers
    Abstract: The optimal layer thicknesses and optimal feedback control function are determined for a symmetric, cross‐ply laminate. The objectives of the optimization are to maximize the biaxial buckling load (design objective) and ...
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