Asymmetric interaction of blast waves and shock waves with a body flying at supersonic velocity

被引：4

作者：

Goloviznin, VP ^{[1
]}

Krasovskaya, IV ^{[1
]}

机构：

[1] Russian Acad Sci, AF Ioffe Physicotech Inst, St Petersburg 194021, Russia

来源：

TECHNICAL PHYSICS | 1999年 / 44卷 / 05期

关键词：

Shock Wave; Blast Wave; Shock Layer; Plane Shock; Interaction Flow;

D O I：

10.1134/1.1259371

中图分类号：

O59 [应用物理学];

学科分类号：

摘要：

The problems of asymmetric interaction of a blunt wedge traveling at supersonic velocity with a cylindrical blast wave from a point explosion and with a plane shock wave are investigated by numerical simulation. The evolution of the interaction flow is analyzed, and data are obtained on how the structure of the shock layer changes. (C) 1999 American Institute of Physics. [S1063-7842(99)00305-0].

引用

页码：493 / 496

页数：4

共 12 条

[1]

CHAMPNEY J, 1982, 820027 AIAA

[2]

GOLOVACHEV YP, 1989, ZH VYCHISL MAT MAT F, V28, P148

[3]

Golovachev Yu. P., 1989, Zhurnal Vychislitel'noi Matematiki i Matematicheskoi Fiziki, V29, P791

[4]

Goloviznin V. P., 1987, Soviet Physics - Technical Physics, V32, P853

[5]

Goloviznin V. P., 1991, Soviet Physics - Technical Physics, V36, P1332

[6]

GOLOVIZNIN VP, 1994, SOV PHYS-TECH PHYS, V39, P540

[7]

Kamenetskii V. F., 1986, NUMERICAL SIMULATION, P104

[8]

KAMENETSKII VF, 1984, IZV AKAD NAUK SSSR M, P141

[9]

KESTENBOIM CS, 1974, POINT EXPLOSION COMP, P255

[10]

NABIEV VU, 1996, PRIKL MAT MEKH, V60, P613

← 1 2 →