NASA NTRS · 20200005874
TPSAS-NF1676L-14336-DND
Abstract
Problem Statement: Develop robust CFD-based methods for rapid design and analysis of supersonic cruise aircraft that are highly efficient, and have a low sonic boom. What is our approach? - Advanced Efficient Analysis / Design Methods - Develop computational algorithms and techniques for rapid high fidelity analysis of supersonic fluid flow phenomena, which will also contribute to multi-fidelity analysis / design tools. - Experimental Validation - Validate concepts for design optimization of both high aerodynamic efficiency and low sonic boom.
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Linda Bangert. TPSAS-NF1676L-14336-DND. https://ntrs.nasa.gov/citations/20200005874
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