Navier-Stokes Optimization of Supersonic Wings with Four Objectives Using Evolutionary Algorithm
By D. Sasaki, S. Obayashi, K. Nakahashi. 2002
105 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics, Global and Planetary Change
View Paper: https://www.semanticscholar.org/paper/33f95b395c59d2055b2159e26a038480b3edc0b6
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In Aerospace Engineering
In Computational Mechanics
Citations in the corpus
- Response surface approximation of pareto optimal front in multi-objective optimization (2004, methodology): “[10,11] used EAs coupled with CFD analysis to design the supersonic wings for multiple objectives.”