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- [6] AERODYNAMIC SHAPE DESIGN OPTIMIZATION FOR TURBOMACHINERY CASCADE BASED ON DISCRETE ADJOINT METHOD PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 7, PTS A-C, 2012, : 1219 - 1228
- [7] Aerodynamic configuration optimization design of hypersonic missile based on discrete adjoint method Jisuan Lixue Xuebao/Chinese Journal of Computational Mechanics, 2012, 29 (02): : 284 - 289
- [8] MULTI-OBJECTIVE AERODYNAMIC AND AEROELASTIC COUPLED DESIGN OPTIMIZATION USING A FULLY TURBULENT DISCRETE ADJOINT HARMONIC BALANCE METHOD PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 10D, 2022,
- [9] Multi-Objective Aerodynamic and Aeroelastic Coupled Design Optimization Using a Full Viscosity Discrete Adjoint Harmonic Balance Method JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2023, 145 (10):