摘要
尾旋预测技术随飞机性能提高而逐步发展完善;
This paper describes with the Improvement of aircraft performance, spin prediction technique is gradually perfected. The tasks and difficulties of spin researches ,as well as spin prediction be considered in all process of the aircraft development ,are explained.
出处
《流体力学实验与测量》
CSCD
1999年第4期32-35,共4页
Experiments and Measurements in Fluid Mechanics
关键词
失速
尾旋
尾旋预测
飞机研制
战斗机
大迎角
stall/spin
spin prediction technique
spin prediction
aircraft development
