Intake effect on drag characteristics of a hemispherical peripheral jet GEM - A preliminary experiment.
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- OTAGIRI Fumiharu
- 名古屋大学工学部航空学教室
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- ANDO Shigenori
- 名古屋大学工学部航空学教室
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- ASAMI Kaiichi
- 川崎重工業株式会社航空機製作所
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- TAKEICHI Naoya
- 川崎重工業株式会社航空機製作所
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- OGAWA Masayuki
- ヤマハ発動機株式会社
Bibliographic Information
- Other Title
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- 半球型周辺噴流GEMの抗力特性に及ぼすIntakeの効果 予備的実験
- ハンキュウガタ シュウヘン フンリュウ GEM ノ コウリョク トクセイ ニ
- A Preliminary Experiment
- 予備的実験
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Description
The drag coefficient of a peripheral jet GEM depends considerably upon the ratio of free stream dynamic pressure to mean cushion pressure. In particular, the drag is significantly less than that evaluated by Chaplin's assumption (parasite drag+ momentum drag). Previously we clarified the existence of a horse-shoe vortex surrounding a GEM model from the bottom of which the air is supplied, and proved the generating mechanism of the "interference thrust". This paper presents a result of preliminary experiments about an intake effect on the GEM external drag. A built-in-fan model ("model 2") is tested in a wind tunnel, and the aerodynamic performance of this model is compared with one for previous model which has no intake ("model 1"). The configuration of model 2 is selected so that the separation of the momentum drag from the external drag may be as reasonable as possible. Both model are hemispherical.
Journal
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- Aeronautical and Space Sciences Japan
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Aeronautical and Space Sciences Japan 34 (387), 222-230, 1986
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282679483729280
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- NII Article ID
- 130003782698
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- NII Book ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL BIB ID
- 3079570
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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