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Simulation-Driven Aerodynamic Design Using Variable-Fidelity Models
This paper presents a historical perspective on the development and application of aerodynamic shape optimization (ASO) methods for supersonic aircraft design. The motivation for using ASO for supersonic transport design is discussed. The accelerated research and development that several ASO methods underwent during the NASA High Speed Research Program is presented. The various ASO algorithms are compared to facilitate an understanding of the proper application of these methods. The continueddoi:10.1142/9781783266296_0002 fatcat:y545vhdwevcexbj6gvy6vbubai