摘要: The General Rotorcraft Aeromechanical Stability Program (GRASP) was developed to analyse the steady-state and linearized dynamic behavior of rotorcraft in hovering and axial flight conditions. Because of the nature of problems GRA... 展开
作者 | Hinnant, H. E. Hodges, D. H. | ||
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原报告号 | ADA1823244 | 总页数 | 11 |
主办者 | Non Paid ADAS | ||
报告分类号 | [51A - Aerodynamics51C - Aircraft] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Hovering Cantilever beams Flight Deformation Dynamics Linearity Rotary wing aircraft Geometric forms Nonlinear systems Displacement Nonlinear analysis Rotor blades(Rotary wings) Deflection Mass Static tests Dynamic tests Rotation Dynamic response Experimental data Correlation Aerodynamic stability Vertical orientation GRASP(General Rotorcraft Aeromechanical Stability Program) Aeromechanical stability Blade tips |