GLOBAL OPTIMAL DESIGN OF TWO AEROSPACE VEHICLES

被引：0
|
作者：
Nastase, A. [1 ]
机构：
[1] Rhein Westfal TH Aachen, RWTH, Aerodynam Flight, Templergraben 55, D-52062 Aachen, Germany
来源：
COUPLED PROBLEMS IN SCIENCE AND ENGINEERING VII (COUPLED PROBLEMS 2017) | 2017年
关键词：
Supersonic Flow; Global Shape Optimization; Solutions for Three-dimensional Hyperbolic PDEs; Meshless; Hybrid Solutions for Navier-Stokes PDEs;
D O I：
暂无
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
A variant of Saenger project is proposed. It is composed of two global optimized and fully-integrated models namely a suborbital small one LEO in form of Catamaran almost blended with two central fuselages almost embeded in the wing thickness and a greater one geostationary one GEO also in form of Catamaran almost blended with two fuselages almost embeded in the wing thickness but located almost parallel to the leading edges, far from the central part of the wing in order to allow the up and go of the LEO in its central part.
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页码：876 / 886
页数：11
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