書誌事項
- タイトル別名
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- Research on the Axisymmetric Flow through an Axial-Flow Turbo-Machine : 2nd Report, Axisymmetric Flow at Design Point in Multistage Turbo-Machines of Various Vortex Types
- ジクリュウ ターボ キカイ ハネグルマ ノ ジク タイショウリュウ ニ ツイテ 2
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In this report, the author has treated the axisymmetric flow at design point in multistage turbo-machines of various vortex types, such as the constant reaction type and the exponential type, using a similar method to that described in 1st Report. Regarding the axisymmetric flow through an axial-flow turbo-machine, the radial equilibrium theory and the actuator disc theory have been expounded, but the effects of impeller breadth and blade shape have not been considered in these theories. The method described in the present paper eliminates the above mentioned disadvantages. Numerical examples are shown comparing with the results calculated on the basis of the above mentioned theories.
収録刊行物
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- 日本機械学會論文集
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日本機械学會論文集 29 (207), 1792-1800, 1963
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390001205158900480
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- NII論文ID
- 110002351958
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- NII書誌ID
- AN00187419
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- ISSN
- 21859485
- 00290270
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- NDL書誌ID
- 9151281
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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
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- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可