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Rapid Aerodynamic Shape Optimization With Payload Size Constraints for Hypersonic Vehicle

Nowadays, aerodynamic shape optimization of the hypersonic vehicle is mostly optimized for local details such as the wing. In the overall shape optimization, the conceptual design of the vehicle is more common, in which the shape is described in fewer parameters and optimized roughly. Meanwhile, in...

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Gorde:
Xehetasun bibliografikoak
Egile Nagusiak: Wuyu Peng, Zhiwei Feng, Tao Yang
Formatua: Artigo
Hizkuntza:Inglês
Argitaratua: IEEE 2019-01-01
Saila:IEEE Access
Gaiak:
Sarrera elektronikoa:https://ieeexplore.ieee.org/document/8736866/
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