抄録
Numerical analysis on an aerodynamic structure of a laminar boundary layer diffusion flame over a horizontal flat plate has been done, taking into account a local pressure gradient in a boundary layer. The calculations were carried out, using a 'Simpler' algorithm. A flame sheet approximation was applied to describe the combustion process. When the flame is formed, the pressure field in the boundary layer is varied locally and the streamwise pressure gradient is formed even if effects of gravity or of acceleration of the free stream velocity are not taken into account. This streamwise pressure gradient induces the velocity overshoot. Furthermore, the numerical calculation, taking into account the effects of gravity and the free stream acceleration in the present equations, shows good agreement with the corresponding experimental results.
| 元の言語 | English |
|---|---|
| ページ（範囲） | 3787-3793 |
| ページ数 | 7 |
| ジャーナル | Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B |
| 巻 | 52 |
| 発行部数 | 483 |
| 出版物ステータス | Published - 1986 11 |
| 外部発表 | Yes |
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ASJC Scopus subject areas
- Mechanical Engineering
これを引用
AERODYNAMIC STRUCTURE OF A LAMINAR BOUNDARY LAYER DIFFUSION FLAME OVER A HORIZONTAL FLAT PLATE. / Ueda, Toshihisa; Mizomoto, Masahiko.
：: Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 巻 52, 番号 483, 11.1986, p. 3787-3793.研究成果: Article
}
TY - JOUR
T1 - AERODYNAMIC STRUCTURE OF A LAMINAR BOUNDARY LAYER DIFFUSION FLAME OVER A HORIZONTAL FLAT PLATE.
AU - Ueda, Toshihisa
AU - Mizomoto, Masahiko
PY - 1986/11
Y1 - 1986/11
N2 - Numerical analysis on an aerodynamic structure of a laminar boundary layer diffusion flame over a horizontal flat plate has been done, taking into account a local pressure gradient in a boundary layer. The calculations were carried out, using a 'Simpler' algorithm. A flame sheet approximation was applied to describe the combustion process. When the flame is formed, the pressure field in the boundary layer is varied locally and the streamwise pressure gradient is formed even if effects of gravity or of acceleration of the free stream velocity are not taken into account. This streamwise pressure gradient induces the velocity overshoot. Furthermore, the numerical calculation, taking into account the effects of gravity and the free stream acceleration in the present equations, shows good agreement with the corresponding experimental results.
AB - Numerical analysis on an aerodynamic structure of a laminar boundary layer diffusion flame over a horizontal flat plate has been done, taking into account a local pressure gradient in a boundary layer. The calculations were carried out, using a 'Simpler' algorithm. A flame sheet approximation was applied to describe the combustion process. When the flame is formed, the pressure field in the boundary layer is varied locally and the streamwise pressure gradient is formed even if effects of gravity or of acceleration of the free stream velocity are not taken into account. This streamwise pressure gradient induces the velocity overshoot. Furthermore, the numerical calculation, taking into account the effects of gravity and the free stream acceleration in the present equations, shows good agreement with the corresponding experimental results.
UR - http://www.scopus.com/inward/record.url?scp=0022811471&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0022811471&partnerID=8YFLogxK
M3 - Article
AN - SCOPUS:0022811471
VL - 52
SP - 3787
EP - 3793
JO - Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
JF - Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
SN - 0387-5016
IS - 483
ER -