Erosive burning of a solid propellant in a supersonic flow

被引：1

作者：

Arkhipov, VA ^{[1
]}

Zimin, DA ^{[1
]}

机构：

[1] Tomsk State Univ, Inst Appl Math & Mech, Tomsk 634050, Russia

来源：

COMBUSTION EXPLOSION AND SHOCK WAVES | 1998年 / 34卷 / 01期

关键词：

Mach Number; Supersonic Flow; Solid Propellant; Critical Cross Section; Erosion Coefficient;

D O I：

10.1007/BF02671818

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

We present results of an experimental study of burning of a ballistite solid propellant (gun powder Ii) in a supersonic how. It is shown that the criterial dependence of the erosion coefficient on the Vilyunov parameter obtained on the basis of experimental results in a subsonic and a supersonic how describes satisfactorily experimental data for a supersonic flow in the examined range of Mach numbers M = 1-2.8 as well. A more correct approximation formula for the range of parameters considered is derived. The specific features of the how along the surface of a solid propellant at M > 1 is analyzed, and this analysis has revealed some problems in the interpretation of experimental data.

引用

页码：55 / 57

页数：3

共 50 条

[41] Solid-propellant gas generators with a gas flow rate stabilization system [J].

S. A. Rashkovskii ;

Yu. M. Milekhin ;

A. V. Fedorychev .

Doklady Chemistry, 2015, 463 :189-193

[42] Cross-flow effect on combustion of a solid propellant with harmonically varying pressure [J].

B. V. Novozhilov .

Combustion, Explosion, and Shock Waves, 2007, 43 :429-434

[43] Solid-propellant gas generators with a gas flow rate stabilization system [J].

Rashkovskii, S. A. ;

Milekhin, Yu M. ;

Fedorychev, A. V. .

DOKLADY CHEMISTRY, 2015, 463 :189-193

[44] Cross-flow effect on combustion of a solid propellant with harmonically varying pressure [J].

Novozhilov, B. V. .

COMBUSTION EXPLOSION AND SHOCK WAVES, 2007, 43 (04) :429-434

[45] Application of high burning rate propellant to impulsive microthruster [J].

Li, SP ;

Zhang, P .

THEORY AND PRACTICE OF ENERGETIC MATERIALS, VOL 5, PARTS A AND B, 2003, :620-623

[46] Effect of tension of a composite propellant on its burning rate [J].

S. A. Rashkovsky ;

Yu. M. Milyokhin ;

A. N. Klyuchnikov ;

A. V. Fedorychev .

Combustion, Explosion, and Shock Waves, 2009, 45 :678-685

[47] Research on Solid Propellant for MEMS-Based Solid Propellant Micro-thruster [J].

Zhang Bin ;

Mao Genwang ;

Xia Quangqing ;

Hu Songqi ;

Wu Suli .

THEORY AND PRACTICE OF ENERGETIC MATERIALS (VOL IX), PROCEEDINGS OF THE 2011 INTERNATIONAL AUTUMN SEMINAR ON PROPELLANTS, EXPLOSIVES AND PYROTECHNICS, 2011, :626-629

[48] Effect of tension of a composite propellant on its burning rate [J].

Rashkovsky, S. A. ;

Milyokhin, Yu. M. ;

Klyuchnikov, A. N. ;

Fedorychev, A. V. .

COMBUSTION EXPLOSION AND SHOCK WAVES, 2009, 45 (06) :678-685

[49] PRANDTL-MEYER REFLECTION FOR SUPERSONIC FLOW PAST A SOLID RAMP [J].

Bae, Myoungjean ;

Chen, Gui-Qiang ;

Feldman, Mikhail .

QUARTERLY OF APPLIED MATHEMATICS, 2013, 71 (03) :583-600

[50] Spatial linear analysis of the flow in a solid rocket motor with burning walls [J].

Massa, L. .

COMBUSTION AND FLAME, 2009, 156 (04) :865-888

← 1 2 3 4 5 →