Stagnation and Jump Phenomenon of Separation Point by Step inside LE-7A Engine Nozzle
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- Watanabe Yasuhide
- 宇宙航空研究開発機構宇宙基幹システム本部
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- Sakazume Norio
- 宇宙航空研究開発機構宇宙基幹システム本部
Bibliographic Information
- Other Title
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- LE-7Aエンジンノズル内段差による剥離の停滞とジャンプの現象
- LE 7A エンジン ノズルナイ ダンサ ニ ヨル ハクリ ノ テイタイ ト ジャンプ ノ ゲンショウ
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Description
At an early stage of development, LE-7A engine suffered from high side loads. One of them was caused by the transition between Free Shock Separation (FSS) and Restricted Shock Separation (RSS), and the other was caused by the stagnation and sudden movement (‘jump’) of the separation point at a small step inside the nozzle extension. This paper focuses on this stagnation and jump phenomenon of separation point caused by the step inside LE-7A engine nozzle during the startup and shutdown transients.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 55 (645), 467-473, 2007
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Keywords
Details 詳細情報について
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- CRID
- 1390282679446424960
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- NII Article ID
- 10020089643
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 8984110
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed