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Evaluating Methods of Combustion Performance at Constant Volume of Deterred Propellant and Mixed Charge(PDF)

《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

Issue:
1996年05期
Page:
13-16
Research Field:
Publishing date:

Info

Title:
Evaluating Methods of Combustion Performance at Constant Volume of Deterred Propellant and Mixed Charge
Author(s):
HeXiaojun WangZeshan
School of Chemical Engineering,NUST,Nanjing 210094
Keywords:
propellant s combustion performance closed bomb v essels
PACS:
TQ562.21
DOI:
-
Abstract:
Propellant’s combustion perfo rmance at constant v olume accessed by closed bomb test is the mo st universal method of today. T he relat ionships between parameters received from mathemat ically tr eated p —t curve measured direct ly f rom closed bomb dev ice are based on homo geneous propellant and parallel combustion law . But for mix ed char ge and deterred propellant , this t radit ional method has some limitat io ns. In this paper, the reason causing the limitat ions is analysed and evaluating methods f it for deterred propellant and mixed charge’s combust ion performance at constant volume are adv anced. Applicat ion of all ev aluat ing methods is discussed.

References:

1 罗运军. 低温感包覆火药装药技术的理论与实验研究. [ 博士学位论文] . 南京: 南京理工大学, 1994
2 华东工程学院. 内弹道实验原理. 北京: 国防工业出版社, 1984. 6

Memo

Memo:
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Last Update: 2013-04-11