Control of Operation Mode Transition with Film Cooling in Dual-Bell Nozzles
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- PROSHCHANKA Dzianis
- 大阪大学大学院基礎工学研究科
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- YONEZAWA Koichi
- 大阪大学大学院基礎工学研究科
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- KOGA Hidekazu
- 大阪大学大学院基礎工学研究科
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- TSUKUDA Hiroaki
- 大阪大学大学院基礎工学研究科
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- TSUJIMOTO Yoshinobu
- 大阪大学大学院基礎工学研究科
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- KIMURA Tatsuya
- 三菱重工業(株)名古屋誘導推進システム製作所
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- YOKOTA Kazuhiko
- 青山学院大学理工学部
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- PASINI Angelo
- ピサ大学
Bibliographic Information
- Other Title
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- フィルム冷却によるデュアルベルノズルの運転モード遷移の制御
- フィルム レイキャク ニ ヨル デュアルベルノズル ノ ウンテン モード センイ ノ セイギョ
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Abstract
Dual-bell nozzle is one of the altitude compensation nozzle concepts, which consists of two bell-type nozzle with different geometric area ratios. The dual bell nozzle has two operation modes—a low altitude operation mode and a high altitude operation mode. However, the practical transition between these operation modes occurs at lower nozzle pressure ratio (NPR) than the optimum one. In the present study, the effect of introduction of film-cooling flow into the nozzle is examined in order to control the operation mode transition NPR. The experimental and numerical results show that the operation mode transition can be control by injecting the film cooling flow at appropriate inlet pressure and flow rate. By injecting the film cooling flow, the axial momentum near the wall in the extension part becomes small and the separation point movement becomes slower. As a result, the dip of the thrust coefficient during the operation mode transition becomes smaller.
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 59 (693), 281-289, 2011
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
- 1390001204470681856
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- NII Article ID
- 10030274963
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 11277305
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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