| Item type |
紀要論文 / Departmental Bulletin Paper(1) |
| 公開日 |
2015-03-26 |
| タイトル |
|
|
タイトル |
Solid Propellant Burning Rate Response Functions of Higher Orders |
|
言語 |
en |
| 言語 |
|
|
言語 |
eng |
| 資源タイプ |
|
|
資源タイプ識別子 |
http://purl.org/coar/resource_type/c_6501 |
|
資源タイプ |
departmental bulletin paper |
| 著者 |
高野, 雅弘
丸泉, 春樹
嶋田, 徹
NOVOZHILOV, Boris V.
KOHNO, Masahiro
MARUIZUMI, Haruki
SHIMADA, Toru
|
| 著者所属 |
|
|
|
宇宙科学研究所 |
| 著者所属 |
|
|
|
日産自動車 |
| 著者所属 |
|
|
|
日産自動車 |
| 著者所属（英） |
|
|
|
en |
|
|
Institute of Chemical Physics, Russian Academy of Sciences |
| 著者所属（英） |
|
|
|
en |
|
|
Institute of Space and Astronautical Science |
| 著者所属（英） |
|
|
|
en |
|
|
Nissan Motor Co., Ltd. |
| 著者所属（英） |
|
|
|
en |
|
|
Nissan Motor Co., Ltd. |
| 出版者 |
|
|
出版者 |
宇宙科学研究所 |
| 出版者（英） |
|
|
出版者 |
Institute of Space and Astronautical Science |
| 書誌情報 |
en : The Institute of Space and Astronautical Science report
巻 661,
p. 1-51,
発行日 1996-01
|
| 抄録（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
To study nonlinear behavior phenomena in a solid propellant rocket motor one should consider both nonlinear acoustic field and nonlinear interaction between acoustic field and combustion process. The former topic has been discussed in literature rather fully. The latter is not a new one but is not studied in detail. In the work presented a new concept of the higher order burning rate response function to acoustic oscillation with several modes is introduced. Analytical calculations are performed in the framework of Z-N theory. Short introduction in this theory is given. The physical-chemical basis of a very high oscillatory quality of condensed system combustion are discussed. In connection with wide use of highly metallized propellants the linear response function of such propellants is calculated. Two most important examples of the first harmonic self-interaction and the first and second modes interaction are obtained analytically. A relative role of the linear and the higher order response functions is discussed. It is shown that nonlinear effects in combustion must be included in solving solid rocket nonsteady behavior problem. |
| ISSN |
|
|
収録物識別子タイプ |
ISSN |
|
収録物識別子 |
0285-6808 |
| 書誌レコードID |
|
|
収録物識別子タイプ |
NCID |
|
収録物識別子 |
AA10632072 |
| 資料番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
資料番号: SA0035219000 |
SA0035219.pdf (2.2 MB)
