FULL-SCALE WIND-TUNNEL INVESTIGATION OF THE ADVANCED TECHNOLOGY LIGHT TWIN-ENGINE AIRPLANE (ATLIT).

被引：0
|
作者：
Hassell Jr., James L.
Newsom Jr., William A.
Yip, Long P.
机构：
来源：
NASA Technical Paper | 1980年 / 1591期
关键词：
D O I：
暂无
中图分类号：
V27 [各类型航空器]; V24 [航空仪表、航空设备、飞行控制与导航];
学科分类号：
082503 ;
摘要：
An investigation has been conducted in the Langley Full-Scale Tunnel to evaluate the aerodynamic performance, stability, and control characteristics of the Advanced Technology Light Twin-Engine airplane (ATLIT). Data were measured over an angle-of-attack range from minus 4 degree to 20 degree for various angles of sideslip between minus 5 degree and 15 degree at Reynolds numbers of 2. 30 multiplied by 10**6 and 3. 50 multiplied by 10**6 for various settings of power and flap deflection. Measurements were also made by means of special thrust-torque balances to determine the installed propeller characteristics.
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