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Experimental verification of the rudder-free stability theory for an airplane model equipped with a rudder having positive floating tendencies and various amounts of friction

机译：配备有具有正浮动倾向和不同摩擦力的舵的飞机模型的无舵稳定性理论的实验验证

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Maggin, Bernard;
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年度 1947
页码 1-25
总页数 25
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIRPLANES - FAIRCHILD R2K-1 (EXPERIMENTAL) WIND TUNNEL TESTS (NACA FREE-FLIGHT-1; RUDDERS, BALANCED; OSCILLATIONS, LATERAL- FAIRCHILD R2K-1; RUDDERS- FAIRCHILD R2K-1; RUDDER CONTROLS- FAIRCHILD R2K-1; STABILITY - FAIRCHILD R2K-1;

机译：飞机 - FaIRCHILD R2K-1（实验）风洞测试（NaCa FREE-FLIGHT-1; RUDDERs，BaLaNCED;振荡，LaTERaL-FaIRCHILD R2K-1; RUDDERs-FaIRCHILD R2K-1; RUDDER CONTROLs- FaIRCHILD R2K-1;稳定性 - FaIRCHILD R2K-1;

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8. Experimental Verification of the Rudder-Free Stability Theory for an Airplane Model Equipped with a Rudder Having Positive Floating Tendencies and Various Amounts of Friction [R] . Maggin, B. 1947

机译：一个飞机模型舵免费稳定性理论的实验验证配备了舵具有正浮倾向和摩擦的不同量的

Experimental verification of the rudder-free stability theory for an airplane model equipped with a rudder having positive floating tendencies and various amounts of friction

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