書誌事項
- タイトル別名
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- Test Facility and the Available Inlet Flow Condition to Transonic Radial Diffusers
- センオンソク エンシン ディフューザ シケン ソウチ ト ディフューザ エ ノ
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抄録
In order to supply the flow field to transonic radial diffusers, a transonic centrifugal impeller with backward blade angle of 40 deg was designed and produced on the basis of the data base accumulated through the authors' experimental study on a radial impeller. In the present paper, the impeller was tested without a diffuser, the flow conditions at the exit of the impeller were evaluated from the test data for impeller characteristics, and the basic data for designing test diffusers are presented. It is concluded that it is possible to pursue the experimental work on diffusers in the range of 21 deg to 11.6 deg in flow angle and up to 1.31 in Mach number using the present test facility.
収録刊行物
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- 九州大学機能物質科学研究所報告
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九州大学機能物質科学研究所報告 1 (1), 91-96, 1987-12-28
九州大学機能物質科学研究所
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詳細情報 詳細情報について
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- CRID
- 1390572174789015680
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- NII論文ID
- 110006177308
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- NII書誌ID
- AN10060378
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- ISSN
- 09143793
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- DOI
- 10.15017/6519
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- HANDLE
- 2324/6519
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- NDL書誌ID
- 3193171
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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
- IRDB
- NDL
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用可