...To reduce the wave resistance that occurs at supersonic speeds, it is best to make the wing long and slender, and if possible, make the sweepback angle of the leading edge sharper than the angle of the shock wave. For this reason, delta wings, which combine a sharp sweepback angle with a small aspect ratio, are often used in supersonic aircraft (Figure 6-f). The aerodynamic center of a delta wing is located at about 50% of the aerodynamic mean chord (about 2/3 of the way from the center chord) at both subsonic and supersonic speeds, and has the advantage of not moving much. *Some of the terminology that mentions "delta wing" is listed below. Source | Heibonsha World Encyclopedia 2nd Edition | Information |
…また超音速で生ずる造波抵抗を減らすには,翼を前後に細長い形とするほか,できれば前縁の後退角を衝撃波の角度以上に鋭くするのがよい。そこで鋭い後退角と小アスペクト比の組合せで得られる三角翼delta wing(デルタ翼ともいう)が,超音速機に多く用いられている(図6-f)。三角翼はその空力中心が,亜音速でも超音速でも空力平均翼弦の約50%(中央翼弦の前から約2/3)にあって,あまり動かないという利点もある。… ※「delta wing」について言及している用語解説の一部を掲載しています。 出典|株式会社平凡社世界大百科事典 第2版について | 情報 |
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