Toward the Realization of a Highly Integrated, Multidisciplinary, Multifidelity Design Environment
Authors:
- 6 January 2019
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 29 references indexed in Scilit:
- Aeroelastic Design Optimization using a Multifidelity Quasi-Newton Method2018
- Generation of Multi-fidelity, Multi-discipline Air Vehicle Models with the Engineering Sketch Pad2016
- Reevaluating conceptual design fidelity: An efficient supersonic air vehicle design caseProceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2015
- Multi-Parameter Performance Evaluation, the Next Step in Conceptual Design Concept Assessment2015
- Efficient supersonic air vehicle design using the Service-Oriented Computing Environment (SORCER)International Journal for Simulation and Multidisciplinary Design Optimization, 2014
- A physics-based distributed collaborative design process for military aerospace vehicle development and technology assessmentInternational Journal of Agile Systems and Management, 2014
- OpenCSM: An Open-Source Constructive Solid Modeler for MDAO2013
- Efficient Supersonic Air Vehicle Preliminary Conceptual Multi-Disciplinary Design Optimization Results2012
- High Fidelity MDO Process Development and Application to Fighter Strike Conceptual Design2012
- On The Construction of Aircraft Conceptual Geometry for High-Fidelity Analysis and Design2012