抄録
The numerical simulations and analyses based on experimental results were carried out by means of computational fluid dynamics. Before now, many experimental and numerical approaches have been conducted for the model whose cross sectional configuration of the fuselage is an isosceles right triangle. It has high lift at high angle of attacks. With these results, new configurations were created to enhance the aerodynamic characteristics and it was obtained that a lift coefficient is increased. The reasons of its increment are analyzed and they are related to the strength of separation vortex and its position. Also, drag coefficients and pitching moment coefficients are discussed in this paper.
| 元の言語 | 英語 |
|---|---|
| ホスト出版物のタイトル | 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition |
| 出版物ステータス | 出版済み - 12 13 2010 |
| イベント | 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Orlando, FL, 米国 継続期間: 1 4 2010 → 1 7 2010 |
出版物シリーズ
| 名前 | 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition |
|---|
その他
| その他 | 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition |
|---|---|
| 国 | 米国 |
| 市 | Orlando, FL |
| 期間 | 1/4/10 → 1/7/10 |
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All Science Journal Classification (ASJC) codes
- Aerospace Engineering
これを引用
A proposal of new fuselage configurations for realizing reusable launch vehicles. / Ishida, Takuro; Aso, Shigeru; Tani, Yasuhiro.
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010. 2010-1045 (48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition).研究成果: 著書/レポートタイプへの貢献 › 会議での発言
}
TY - GEN
T1 - A proposal of new fuselage configurations for realizing reusable launch vehicles
AU - Ishida, Takuro
AU - Aso, Shigeru
AU - Tani, Yasuhiro
PY - 2010/12/13
Y1 - 2010/12/13
N2 - The numerical simulations and analyses based on experimental results were carried out by means of computational fluid dynamics. Before now, many experimental and numerical approaches have been conducted for the model whose cross sectional configuration of the fuselage is an isosceles right triangle. It has high lift at high angle of attacks. With these results, new configurations were created to enhance the aerodynamic characteristics and it was obtained that a lift coefficient is increased. The reasons of its increment are analyzed and they are related to the strength of separation vortex and its position. Also, drag coefficients and pitching moment coefficients are discussed in this paper.
AB - The numerical simulations and analyses based on experimental results were carried out by means of computational fluid dynamics. Before now, many experimental and numerical approaches have been conducted for the model whose cross sectional configuration of the fuselage is an isosceles right triangle. It has high lift at high angle of attacks. With these results, new configurations were created to enhance the aerodynamic characteristics and it was obtained that a lift coefficient is increased. The reasons of its increment are analyzed and they are related to the strength of separation vortex and its position. Also, drag coefficients and pitching moment coefficients are discussed in this paper.
UR - http://www.scopus.com/inward/record.url?scp=78649862267&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=78649862267&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:78649862267
SN - 9781600867392
T3 - 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
BT - 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
ER -