| Item type |
紀要論文 / Departmental Bulletin Paper(1) |
| 公開日 |
2015-03-26 |
| タイトル |
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|
タイトル |
Generation and Observation of Strong Shock Waves in the Flight Regiemes of AOTV |
|
言語 |
en |
| 言語 |
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|
言語 |
eng |
| 資源タイプ |
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|
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 |
HONMA, Hiroki
TSUKAMOTO, Akira
OHNO, Taroh
TANAKA, Takashi
|
| 著者所属（英） |
|
|
|
en |
|
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Department of Mechanical Engineering, Chiba University |
| 著者所属（英） |
|
|
|
en |
|
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Department of Mechanical Engineering, Chiba University |
| 著者所属（英） |
|
|
|
en |
|
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Department of Mechanical Engineering, Chiba University |
| 著者所属（英） |
|
|
|
en |
|
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Department of Mechanical Engineering, Chiba University |
| 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. S.P. : An Aerodynamics in Relation to an Aeroassisted Orbit Transfer Vehicle
巻 7,
p. 15-25,
発行日 1988-11
|
| 抄録（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
By using a free-piston, double-diaphragm shock tube, strong shock waves around 10 km/s are generated in air of initial pressure 13.3 Pa, corresponding to the flight regiems of AOTV. A system of automatic valve is developed to remove the diaphragm between high-pressure and compression chambers, and its usage results in remarkable improvement for reproducing shock waves with the same strength in the test section, The measured risetime of radiation intensity behind the shock front, as well as the duration of light emission, exhibits good agreement with the data obtained by Allen et al.[2]. Radiation profiles and ion-probe outputs are observed in the center of cross section of the tube and near by the wall. The results show that the contact zone is retarded near by the wall due to effect of boundary layer, though appreciable differences are not observed for front structures. |
| ISSN |
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収録物識別子タイプ |
ISSN |
|
収録物識別子 |
0288-433X |
| 書誌レコードID |
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|
収録物識別子タイプ |
NCID |
|
収録物識別子 |
AA10455137 |
| 資料番号 |
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内容記述タイプ |
Other |
|
内容記述 |
資料番号: SA0033605000 |
SA0033605.pdf (624.2 kB)
