Contouring two-sided asymmetric plane maximum-thrust nozzles

被引：0
|
作者：
A. A. Kraiko
K. S. Pyankov
N. I. Tillyaeva
机构：
[1] Baranov Central Institute of Aviation Motors (CIAM),
来源：
Fluid Dynamics | 2016年 / 51卷
关键词：
asymmetric nozzles; direct optimization methods; genetic algorithms;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The results of the optimal contouring of asymmetric plane nozzles under some additional constraints are presented. One of the constraints is due to the asymmetric arrangement of the unknown nozzles relative to the combustion chamber exit. The investigation is based on the numerical integration of the Reynolds-averaged Navier–Stokes equations and direct optimization methods using genetic algorithms and the representation of the optimized contours in the form of the Bernstein–Bézier curves.
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页码：120 / 125
页数：5
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