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Effects of Tail Wing Area on Model Airplane Endurance Performance.
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- KATO Kanichiro
- 東京大学工学部航空学科
Bibliographic Information
- Other Title
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- 模型飛行機の水平尾翼面積と滞空性能
- モケイ ヒコウキ ノ スイヘイ ビヨク メンセキ ト タイクウ セイノウ
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Description
Trim, static stability and endurance are discussed about the model airplane and simplified formulas are given for them. Also, wing aerodynamic characteristics are reviewed for Reynolds No. at about 104. Combining these, the reason is estimated why model airplanes have larger horizontal tail (relative to wing) than real airplanes.
Journal
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- Aeronautical and Space Sciences Japan
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Aeronautical and Space Sciences Japan 40 (461), 338-345, 1992
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
- 1390282679453917952
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- NII Article ID
- 130003958937
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- NII Book ID
- AN00189072
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- ISSN
- 24241369
- 00214663
- http://id.crossref.org/issn/00214663
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- NDL BIB ID
- 3769545
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL Search
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed