论文信息 - Optimum Aerodynamic Design of Cascades by Using an Adjoint Equation Method - 字舞流文

Optimum Aerodynamic Design of Cascades by Using an Adjoint Equation Method

Feng Liu | Shuchi Yang | F. Liu | Shuchi Yang | Feng Liu

[1] S. Damle,et al. Euler-Based Inverse Method for Turbomachine Blades, Part 2: Three-Dimensional Flows , 2000 .

[2] T. Dang,et al. Euler-based inverse method for turbomachine blades. I - Two-dimensional cascades , 1995 .

[3] Juan J. Alonso,et al. Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers , 1996 .

[4] Antony Jameson,et al. Aerodynamic design via control theory , 1988, J. Sci. Comput..

[5] W. R. Hawthorne,et al. Theory of Blade Design for Large Deflections: Part II—Annular Cascades , 1984 .