Art
J-GLOBAL ID:201902222882478272   Reference number:19A0327818

Dynamic simulation of ignition, combustion, and extinguishment processes of HMX/GAP solid propellant in rocket motor using moving boundary approach

移動境界法を用いたロケットモータにおけるHMX/GAP固体推薬の着火,燃焼,消火プロセスの動的シミュレーション【JST・京大機械翻訳】
Author (6):
Material:
Volume: 201  Page: 129-139  Publication year: 2019 
JST Material Number: C0104A  ISSN: 0010-2180  CODEN: CBFMAO  Document type: Article
Article type: 原著論文  Country of issue: Netherlands (NLD)  Language: ENGLISH (EN)
Abstract/Point:
Abstract/Point
Japanese summary of the article(about several hundred characters).
All summary is available on JDreamIII(charged).
On J-GLOBAL, this item will be available after more than half a year after the record posted. In addtion, medical articles require to login to MyJ-GLOBAL.
Solid propellant burning rate,...
   To see more with JDream III (charged).   {{ this.onShowAbsJLink("http://jdream3.com/lp/jglobal/index.html?docNo=19A0327818&from=J-GLOBAL&jstjournalNo=C0104A") }}
Thesaurus term:
Thesaurus term/Semi thesaurus term
Keywords indexed to the article.
All keywords is available on JDreamIII(charged).
On J-GLOBAL, this item will be available after more than half a year after the record posted. In addtion, medical articles require to login to MyJ-GLOBAL.

Semi thesaurus term:
Thesaurus term/Semi thesaurus term
Keywords indexed to the article.
All keywords is available on JDreamIII(charged).
On J-GLOBAL, this item will be available after more than half a year after the record posted. In addtion, medical articles require to login to MyJ-GLOBAL.
, 【Automatic Indexing@JST】
JST classification (2):
JST classification
Category name(code) classified by JST.
Various explosives and propellants  ,  Combustion in general 

Return to Previous Page