Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm

【Author】

K.Cui;S.C.Hu;T.Y.Gao;X.P.Wang;G.W.Yang;

【Abstract】

<正>This work is concerned with the design of a leading edge for hypersonic vehicles used to minimize the peak heat flux of the leading edge.The leading edge is parameterized by using B-spline curve method.The hypersonic flow field and the heat flux dis-

【Keywords】

heat;Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm;

References

To explore the background and basis of the node document

Springer Journals Database

Total: 0 articles

Similar documents

Documents that have the similar content to the node document

More>>