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    Adaptivity in <i>P</i>‐Version Finite Element Analysis 

    Source: Journal of Structural Engineering:;1983:;Volume ( 109 ):;issue: 010
    Author(s): Prodyot K. Basu; Alberto Peano
    Publisher: American Society of Civil Engineers
    Abstract: Adaptive finite element technology has the potential for reducing the cost of structural analysis significantly. There are two different approaches to improve upon the solution accuracy: (1) By selective mesh refinement ...
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    Higher Order Modeling of Plates by <i>p</i>‐Version of Finite Element Method 

    Source: Journal of Engineering Mechanics:;1993:;Volume ( 119 ):;issue: 006
    Author(s): Nesar U. Ahmed; Prodyot K. Basu
    Publisher: American Society of Civil Engineers
    Abstract: A new
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    Partially Prestressed Composite Beams. II 

    Source: Journal of Structural Engineering:;1987:;Volume ( 113 ):;issue: 009
    Author(s): Prodyot K. Basu; Alfarabi M. Sharif; Nesar U. Ahmed
    Publisher: American Society of Civil Engineers
    Abstract: The behavior of a two‐span composite beam, consisting of a concrete slab shear connected to a steel beam and prestressed near the central support region, was studied experimentally. The test beam was 37 ft (11.28 m) long ...
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    Partially Prestressed Continuous Composite Beams. I 

    Source: Journal of Structural Engineering:;1987:;Volume ( 113 ):;issue: 009
    Author(s): Prodyot K. Basu; Alfarabi M. Sharif; Nesar U. Ahmed
    Publisher: American Society of Civil Engineers
    Abstract: The behavior of partially prestressed composite beams consisting of a concrete slab supported by a steel beam is analytically evaluated. The prestress is introduced in the negative moment regions when the slab acts compositely ...
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    Adaptive Control of Aircraft Wing Flutter by Stress-Induced Stiffness Modification 

    Source: Journal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 004
    Author(s): Mazita Mohd Tahir; Prodyot K. Basu; John R. Veillette
    Publisher: American Society of Civil Engineers
    Abstract: Lightweight unoccupied air vehicles (UAVs) with wide wingspans are especially vulnerable to dynamic instability. Such instability can be contained by using mass and stiffness balancing and the shape and attitude of the ...
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