Nonstationary Motion of Purely Supersonic Wings
نویسندگان
چکیده
منابع مشابه
Multiobjective Aerodynamic Optimization of Supersonic Wings Using Navier-Stokes Equations
The design optimization of a wing for supersonic transport by means of Multiobjective Genetic Algorithm (MOGA) is presented. The objective function is to minimize the drag for transonic cruise, the drag for supersonic cruise and the bending moment at the wing root for the supersonic condition. The wing shape is defined by planform, thickness distributions and warp shapes, in total of 66 design ...
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ژورنال
عنوان ژورنال: Journal of the Aeronautical Sciences
سال: 1951
ISSN: 1936-9956
DOI: 10.2514/8.1946