Bibliographic Information
- Other Title
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- 亜音速翼列近似理論
- アオンソクヨクレツ キンジ リロン
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Abstract
This paper deals with an approximate theory of airfoil cascades in subsonic flow. The theory is developed by the so-called "Interference Method" and the Prandtl-Glauert's approximate theory of airfoil in subsonic flow. The calculated results of some airfoil cascades coincide well with the ones calculated by the "Hodograph Method". The Inverse Problem is also discussed in this paper.
Journal
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- Transactions of the Japan Society of Mechanical Engineers
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Transactions of the Japan Society of Mechanical Engineers 25 (157), 920-927, 1959
The Japan Society of Mechanical Engineers
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Details 詳細情報について
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- CRID
- 1390001205155144704
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- NII Article ID
- 110002456943
- 110002351030
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- NII Book ID
- AN00187419
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- ISSN
- 21859485
- 24242675
- 00290270
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- NDL BIB ID
- 9150436
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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