書誌事項
- タイトル別名
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- Highly Loaded Fan by Using Tandem Cascade Rotor Blade.
- タンデムヨクレツ ニ ヨル ファン ノ コウフカカ
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説明
For axial flow compressors and fans in the aircraft engines higher pressure ratio is required in order to attain the high thrust engines. In this study, the fan with the tandem cascades was introduced to increase the fan pressure ratio. The use of tandem cascades in the fan allows savings in length and weight and therefore a compact fan could be built. The design of fan with tandem cascades and the fan testing were carried out to develop the high pressure ratio fan for the Air Turbo Ramjet (ATR) propulsion system. The ATR is a combined cycle engine which performs like a turbojet engine at subsonic speeds and a ramjet at supersonic speeds. In particular, high fan pressure ratio contributes to increase the engine thrust during subsonic flight at which the engine does not make use of ram effect. The results of the fan testing indicate that the pressure ratio of 2.2 is achieved in single stage fan.
収録刊行物
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- 日本航空宇宙学会論文集
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日本航空宇宙学会論文集 51 (588), 17-22, 2003
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390001204469310080
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- NII論文ID
- 130000146738
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 6440872
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDLサーチ
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