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HyperSizer

HyperSizer is computer-aided engineering (CAE) software used for stress analysis and sizing optimization of metallic and composite structures… Expand
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Papers overview

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2016
2016
Purpose The purpose of this paper is to present a structural design and optimization module for aircraft structures that… Expand
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2011
2011
For the NASA Heavy Launch Vehicle (HLV), substantial weight reduction is possible by designing the Payload Shroud, Interstage… Expand
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2009
2009
With the increasingly widespread application of composite materials,particularly in the aeronautic astronautic industry,the… Expand
2008
2008
This paper outlines a method for the stress analysis of bonded composite corrugated panel facesheet to flange joints. The method… Expand
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2007
2007
A process of performing high fidelity aerospace structural analyses early in the design cycle is presented. The process has been… Expand
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2005
2005
Failure analysis of bonded composite joints is essential to the design of modern aerospace vehicles in which adhesive joints are… Expand
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2003
2003
Abstract : Collier Research Corporation is working with Lockheed Martin Aeronautics (LM Aero) under United States Air Force… Expand
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2002
2002
Abstract : The Air Force Research Laboratory Space Vehicles Directorate (AFRL/VS) is exploring new structural configurations and… Expand
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2001
2001
Abstract : Due to weight and cost goals. a grid-stiffened panel concept is being used for redesign of a structural component on… Expand
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1997
1997
Characteristics of a next generation software product are presented for a coupled MSC/NASTRAN FEA and structural optimization… Expand
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