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Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 3 degree trim and with a 22 1/2 degree angle of dead rise

机译：流体动力冲击载荷随着飞行路径角的变化而变化，棱柱形浮子在3度纵倾时具有22 1/2度的死角

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Batterson, Sidney A;
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年度 1945
页码 1-5
总页数 5
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
FLOATS - IMPACT TANK TESTS (NACA); LANDINGS - SEAPLANES; LOADS - FLOATS;

机译：FLOaTs - 冲击坦克测试（NaCa）;登陆 - 海底;负荷 - 浮子;

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4. An immersion and invariance based speed and rotation angle observer for a class of revolute/prismatic manipulators with two degrees of freedom [C] . Rapp P., Sawodny O., Tarin C. IEEE Annual Conference on Decision and Control . 2013

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5. PHOTOPRODUCTION OF 42.4 MEV POSITIVE PIONS FROM HYDROGEN AT LABORATORY ANGLES BETWEEN 50 AND 170 DEGREES. [D] . BAUM, PAUL MARTIN. 1962

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7. Worse self-reported outcomes in patients with longstanding hip/groin pain and alpha angles ≥60 degrees compared to patients with alpha angles < 60 degrees [O] . I. Kostogiannis, D. Rizvanovic, A. Nageeb Mahmoud, 2017

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8. Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 6 degrees and 9 degrees trim and a 22-1/2 degree angle of dead rise [R] . Stewart, Thelma 1946

机译：流体动力冲击载荷随飞行路径角的变化而变化为6度和9度的棱柱形浮动和22-1 / 2度的死角

Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 3 degree trim and with a 22 1/2 degree angle of dead rise

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