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

页码：1004 / 1015

页数：12

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