Modeling the Flow around a Delta Wing Partially Made of a Permeable Material

被引：0
|
作者：
Lutsky, A. E. [1 ]
Severin, A. V. [1 ]
机构：
[1] Russian Acad Sci, Keldysh Inst Appl Math, Moscow 125047, Russia
来源：
FLUID DYNAMICS | 2024年 / 59卷 / 04期
基金：
俄罗斯科学基金会;
关键词：
delta wing; gas dynamics; computational aerodynamics; porous materials;
D O I：
10.1134/S0015462824602778
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
Mathematical modeling of a supersonic gas flow around a delta wing is carried out for M = 2. A wing made of a conventional solid material is compared to a wing whose leading edge is made of a porous material with a porosity coefficient of 0.6. The influence of a permeable edge on the flow structure and thermal regime is studied.
引用
收藏
页码：1004 / 1015
页数：12
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