transonic flight

The main object of this paper is that the representative comprehensive characteristics of similar parameters at maximum and afterburning conditions of engine , subsonic and transonic flight , i. e. of various maneuvers .

本文旨在通过各种机动飞行，荻得最大状态、加力状态、亚音速和跨音速典型的相似参数综合特性线，利用这些曲线可计算飞机大速度、稳定盘旋，跃升拉起和盘旋上升等一些典型性能。

Research on the modeling of pitching moment coefficient in transonic condition for flight vehicle

飞行器跨声速区俯仰力矩系数建模方法研究

The institutions pay much attention to it stemmed from the fact . Oblique wing aircraft can decrease high transonic and low supersonic flight drag , and improves the aerodynamic efficiency in high speed flight .

因此斜置机翼飞机能够有效地减小飞机在高跨音速和低超音速时的飞行阻力，提高飞机超音速飞行的气动效率。