マッハ数1.88における三角翼胴体結合の揚力・縦揺れモーメントと圧力中心の測定
1962 年 10 巻 97 号 p. 39-42
詳細
1962 年 10 巻 97 号 p. 39-42
Measurements have been made of the lift, pitching moment and center of pressure of delta wing-body combinations at supersonic Mack number 1.88. Conical nose bodies, with cylindrlcal body lengths of 75mm and 150mm, and with delta wing aspect ratios varying systematically from 0.67 to 3.33, were investigated. The purpose of this study was to describe in a systematic manner the variation of the wing-body combination aerodynamic characteristics with aspect ratio and body length. These data are in reasonable agreement with the theoretical values predicted by G.K. Morikawa, F.H. Tsien and T. Nonweiler.
