首页> 美国政府科技报告 >Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Fairchild Lark Pilotless-Aircraft Configuration. Standard Configuration with Wing Flaps Deflected 60 deg and Model Having Tail in Line with Wings. TED No. NACA 2387
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Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Fairchild Lark Pilotless-Aircraft Configuration. Standard Configuration with Wing Flaps Deflected 60 deg and Model Having Tail in Line with Wings. TED No. NACA 2387

机译:的仙童云雀无人驾驶飞机配置的0.5比例模型的纵向稳定性和控制特性的试飞评估。标准配置带襟翼攻击偏斜60度和模式具有线路尾部有翅膀。 TED号NaCa 2387

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