sweepforward
1. sweepforward angle
前刮角
2. sweepforward wing
前掠翼
3. A fixed-geometry two dimensional mixed compression supersonic inlet with sweepforward high-light is tested in a wind tunnel.The inlet is designed in an "X" type missile configuration.
摘要针对一种定几何二元倒置"X"型布局的混压式进气道进行了风洞吹风实验,得到了进气道的性能并进行了分析。