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Floating characteristics of a plain and a horn-balanced rudder at spinning attitudes as determined from rotary tests on a model of a typical low-wing personal-owner airplane

机译：通过在典型的低翼个人所有者飞机模型上的旋转测试确定的平面和喇叭平衡舵的浮动特性

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作者
Bihrle, William, Jr;
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年度 1951
页码 1-94
总页数 94
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
RUDDERS, BALANCED - HORN; RUDDERS - OSCILLATIONS; SPINNING CHARACTERISTICS - EFFECT OF WING-TAIL COMBINATIONS; SPINNING CHARACTERISTICS - EFFECT OF TAIL SURFACES; SPINNING - RECOVERY; RUDDERS - HINGE MOMENTS; INTERFERENCE - TAIL SURFACES & WINGS; SIDESLIPPING; WIND TUNNEL TESTS - NACA - FREE-SPINNING (20 FEET); SPINNING TESTS - AIRPLANES, LIGHT;

机译：RUDDERs，BaLaNCED - HORN; RUDDERs - OsCILLaTIONs;纺纱特性 - 翼尾组合的影响;纺纱特性 - 尾部表面的影响;纺纱 - 恢复; RUDDERs - HINGE mOmENTs;干涉 - 尾部表面＆amp; WINGs;侧滑;风洞隧道测试 - NaCa - 自由旋转（20英尺）;纺纱试验 - 飞机，轻型;
入库时间 2022-08-29 11:20:00

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Floating characteristics of a plain and a horn-balanced rudder at spinning attitudes as determined from rotary tests on a model of a typical low-wing personal-owner airplane

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