模型飛行機の水平尾翼面積と滞空性能
1992 年 40 巻 461 号 p. 338-345
詳細
1992 年 40 巻 461 号 p. 338-345
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.
