Comparative analysis of methods for measuring the transient burning rate. II. Research results

Abstract

This paper presents the results of measurements of the transient burning rate of homogeneous and model composite solid propellants during sudden depressurization of a semi-enclosed volume using two independent methods - high-speed photography and a method based on solving the inverse problem of interior ballistics. A comparative analysis of the results shows that the methods are mutually complementary.

Original language	English
Pages (from-to)	570-577
Number of pages	8
Journal	Combustion, Explosion and Shock Waves
Volume	46
Issue number	5
DOIs	https://doi.org/10.1007/s10573-010-0075-8
Publication status	Published - 1 Sep 2010

Keywords

depressurization
half-closed volume
high-speed photography
hot-spot pulsating combustion regime
inverse problem of interior ballistics
solid propellants
transient burning rate

ASJC Scopus subject areas

Chemistry(all)
Chemical Engineering(all)
Fuel Technology
Energy Engineering and Power Technology
Physics and Astronomy(all)

Access to Document

10.1007/s10573-010-0075-8

Fingerprint Dive into the research topics of 'Comparative analysis of methods for measuring the transient burning rate. II. Research results'. Together they form a unique fingerprint.

Cite this

@article{da5b3a2b8c154c4fb7b5e3ebd0b3d911,

title = "Comparative analysis of methods for measuring the transient burning rate. II. Research results",

abstract = "This paper presents the results of measurements of the transient burning rate of homogeneous and model composite solid propellants during sudden depressurization of a semi-enclosed volume using two independent methods - high-speed photography and a method based on solving the inverse problem of interior ballistics. A comparative analysis of the results shows that the methods are mutually complementary.",

keywords = "depressurization, half-closed volume, high-speed photography, hot-spot pulsating combustion regime, inverse problem of interior ballistics, solid propellants, transient burning rate",

author = "Arkhipov, {V. A.} and Bondarchuk, {S. S.} and Korotkikh, {A. G.}",

year = "2010",

month = sep,

day = "1",

doi = "10.1007/s10573-010-0075-8",

language = "English",

volume = "46",

pages = "570--577",

journal = "Combustion, Explosion and Shock Waves",

issn = "0010-5082",

publisher = "Springer New York",

number = "5",

}

TY - JOUR

T1 - Comparative analysis of methods for measuring the transient burning rate. II. Research results

AU - Arkhipov, V. A.

AU - Bondarchuk, S. S.

AU - Korotkikh, A. G.

PY - 2010/9/1

Y1 - 2010/9/1

N2 - This paper presents the results of measurements of the transient burning rate of homogeneous and model composite solid propellants during sudden depressurization of a semi-enclosed volume using two independent methods - high-speed photography and a method based on solving the inverse problem of interior ballistics. A comparative analysis of the results shows that the methods are mutually complementary.

AB - This paper presents the results of measurements of the transient burning rate of homogeneous and model composite solid propellants during sudden depressurization of a semi-enclosed volume using two independent methods - high-speed photography and a method based on solving the inverse problem of interior ballistics. A comparative analysis of the results shows that the methods are mutually complementary.

KW - depressurization

KW - half-closed volume

KW - high-speed photography

KW - hot-spot pulsating combustion regime

KW - inverse problem of interior ballistics

KW - solid propellants

KW - transient burning rate

UR - http://www.scopus.com/inward/record.url?scp=78049342032&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=78049342032&partnerID=8YFLogxK

U2 - 10.1007/s10573-010-0075-8

DO - 10.1007/s10573-010-0075-8

M3 - Article

AN - SCOPUS:78049342032

VL - 46

SP - 570

EP - 577

JO - Combustion, Explosion and Shock Waves

JF - Combustion, Explosion and Shock Waves

SN - 0010-5082

IS - 5

ER -