107 パワード・リフト機模型の後流測定
書誌事項
- タイトル別名
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- Wake Measurement on Aircraft Model with USB Powered High Lift System
抄録
The aircraft employing the Upper Surface Blowing(USB) system as a poweredlift technology makes use of the energy of the engine exhoust to augument wing lift. The aircraft with the USB system achieves higher powered-lift by turning full downward the engine exhaust flow. To studying powered-lift characteristics, the wakes of the semi-span aircraft model with USB Powered high lift system were measured by a taversing wake rake with 5-pitot tube in NAL 2×2m Gust Wind Tunnel.<BR>In this report, the characteristics for the wake having different turning angle of exhaust flow are described.
収録刊行物
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- 可視化情報学会誌
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可視化情報学会誌 13 (Supplement2), 35-38, 1993
社団法人 可視化情報学会
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詳細情報 詳細情報について
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- CRID
- 1390001204619366400
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- NII論文ID
- 130003442959
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- ISSN
- 1884037X
- 09164731
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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
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可