書誌事項
- タイトル別名
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- The Effect of the Air Humidity on the Cascade Performance in the Suction Type Shock Tunnel
- タイキ スイコミシキ ショウゲキ フウドウ オ モチイタ ヨクレツ ジッケン
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説明
The effects of water vapor condensation on the transonic turbine cascade flow in a suction type shock tunnel are investigated by the optical methods and by the wake traverse method using the Pitot comb with silicon oil containing tubes. It is shown that the flow pattern and the downstream total pressures are influenced considerably by the condensation for the supersonic exit flow. The traverse test results using the shock tunnel with dried air (Dew point Td=-10°C) show fairly good agreement with the experimental results in an ordinary blow-down type wind tunnel, which are considered to have almost no effects of water vapor condensation.
収録刊行物
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- 日本航空宇宙学会誌
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日本航空宇宙学会誌 30 (337), 83-90, 1982
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
- 1390001204505761664
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- NII論文ID
- 130003958453
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- NII書誌ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL書誌ID
- 2440325
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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
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可