Helicopter Roll-On Takeoff Simulation

著录项

• 来源
  《Journal of the American Helicopter Society》 |2011年第1期|p.012003.1-012003.15|共15页
• 作者

  K. Enciu; A. Rosen;

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• 作者单位

  Aircraft Engineering Department Israeli Air Force, Tel Aviv, Israel;

  Faculty of Aerospace Engineering Technion—Israel Institute of Technology, Haifa, Israel;

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• 收录信息
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  A_(1c), B_(1c), θ_0: lateral, longitudinal, and collective pitch; Aij: elements of a transfer matrix from (E) coordinate system to (F) coordinate system; a,h_p,h_s,l_p,l_s, R_(cs),s,s_t,y_p,y_s, △: main landing gear geometric properties; aZw: vertical component of acceleration of main rotor hub in wind (W) coordinate system; et al;

  机译：A_（1c）;B_（1c）;θ_0：横向;纵向和整体螺距;Aij：从（E）坐标系到（F）坐标系的传递矩阵的元素;a;h_p;h_s;l_p;l_s;R_（cs）;s;s_t;y_p;y_s;△：主起落架的几何特性;aZw：风（W）坐标系中主转子轮毂加速度的垂直分量;等;