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Simplified procedures for estimating flapwise bending moments on helicopter rotor blades. Part 1 - Procedures and charts

机译：估算直升机旋翼叶片襟翼弯矩的简化程序。第1部分 - 程序和图表

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Estimation of flapwise bending moments on helicopter rotor blades

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作者
Landgrebe, A. J.;
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年度 1969
页码 1-463
总页数 463
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
BENDING MOMENTS; FLAPS (CONTROL SURFACES); HELICOPTER DESIGN; ROTARY WINGS; APPROXIMATION; COEFFICIENTS; COMPUTER PROGRAMS; GRAPHS (CHARTS); NUMERICAL ANALYSIS; TORSIONAL STRESS; TRANSFER FUNCTIONS;

机译：弯曲的时刻; FLaps（控制表面）;直升机设计;旋转翼;近似;系数;电脑程序;图表（图表）;数值分析;扭转应力;转移功能;

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5. Effect of pitch angle and rotor speed on bending-bending elastic coupling of the CH149 Cormorant helicopter tail rotor blades. [D] . Laliberte, Maryse. 2012

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6. Bias in Estimates of Quantitative-Trait–Locus Effect in Genome Scans: Demonstration of the Phenomenon and a Method-of-Moments Procedure for Reducing Bias [O] . David B. Allison, Jose R. Fernandez, Moonseong Heo, 2002

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7. On the Flapwise Bending Characteristics of Helicopter Rotor Blade [O] . Matsuoka Kenji 1961

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Simplified procedures for estimating flapwise bending moments on helicopter rotor blades. Part 1 - Procedures and charts

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