Pressure and velocity fields of spatial cross section on an aircraft model with strakewing and double vertical tails were measured using a seven hole probe.
采用七孔探针对一种边条翼双垂尾布局的飞机模型进行了空间压力场和速度场的测量。
2
An experimental study of the effects of the twin vertical fins position and twist strakewing on a fighter aerodynamic characteristics was performed in the wind tunnel.
针对边条弯扭及改变双立尾展向位置对全机纵横向气动特性的影响进行了试验研究。
3
An idea for the aerodynamic design of a strake-wing is proposed from the control standpoint with utilization of vortex and separated flows.