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The purpose of this paper is to present a structural design and optimization module for aircraft structures that… Expand For the NASA Heavy Launch Vehicle (HLV), substantial weight reduction is possible by designing the Payload Shroud, Interstage… Expand With the increasingly widespread application of composite materials,particularly in the aeronautic astronautic industry,the… Expand This paper outlines a method for the stress analysis of bonded composite corrugated panel facesheet to flange joints. The method… Expand A process of performing high fidelity aerospace structural analyses early in the design cycle is presented. The process has been… Expand Failure analysis of bonded composite joints is essential to the design of modern aerospace vehicles in which adhesive joints are… Expand Abstract : Collier Research Corporation is working with Lockheed Martin Aeronautics (LM Aero) under United States Air Force… Expand Abstract : The Air Force Research Laboratory Space Vehicles Directorate (AFRL/VS) is exploring new structural configurations and… Expand Abstract : Due to weight and cost goals. a grid-stiffened panel concept is being used for redesign of a structural component on… Expand Characteristics of a next generation software product are presented for a coupled MSC/NASTRAN FEA and structural optimization… Expand