Aerodynamic Optimization Design of Supersonic Wing Based on Discrete Adjoint
Reducing fuel consumption and improving the economy by effectively reducing cruising drag is the main objective of the aerodynamic design of supersonic civil aircraft. In this paper, the aerodynamic optimization design system based on the Reynolds-Averaged Navier–Stokes (RANS) equation and discrete...
| Main Authors: | , , , , , |
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| פורמט: | Article |
| שפה: | English |
| יצא לאור: |
MDPI AG
2023-04-01
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| סדרה: | Aerospace |
| נושאים: | |
| גישה מקוונת: | https://www.mdpi.com/2226-4310/10/5/420 |