The paper proposes the technique based on solutions of the Reynolds-averaged Navier–Stokes (RANS) equations for selecting the optimal aerodynamic configuration of the wing at the early design stages. The general optimization algorithm is presented taking into account a great number of design variables and constraints. A parameterization approach is presented that allows the efficient manipulation of the wing geometry. The results of aerodynamic optimization of the isolated wing of the second-generation supersonic passenger aircraft are presented.
Optimization of the Aerodynamic Configuration of the Isolated Wing for the Second-Generation Supersonic Passenger Aircraft
Russ. Aeronaut.
Russian Aeronautics ; 67 , 1 ; 70-79
2024-03-01
10 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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