Analysis of Flexible Aircraft Dynamics Using Bifurcation Methods

著录项

• 来源
  《Journal of guidance, control, and dynamics》 |2011年第3期|p.795-809|共15页
• 作者

  N. Baghdadi; M. H. Lowenberg; A. T. Isikveren;

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• 作者单位

  University of Bristol, Bristol, England BS8 1TR, United Kingdom,Department of Aerospace Engineering;

  University of Bristol, Bristol, England BS8 1TR, United Kingdom,Department of Aerospace Engineering;

  University of Bristol, Bristol, England BS8 1TR, United Kingdom,Department of Aerospace Engineering, currently Head Radical Aircraft Concepts, Bauhaus Luftfahrt, D-80807 Miinchen, Germany;

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• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  b; wing span, m; C_(mo), C_(z0); pitching moment and normal force coefficients; C_M(.), C_X(.),; pitching moment, axial and normal force; C_z(.); derivatives due to (.); C_(.)~ni; generalized aerodynamic derivative due to (.) associated with the ith elastic mode; et al;

  机译：b;翼展;米;C_（mo）;C_（z0）;俯仰力矩和法向力系数;C_M（。）;C_X（。）、;俯仰力矩;轴向力和法向力;C_z（。）;（。）衍生的;C _（。）〜ni;由于（。）与第i个弹性模态相关的广义空气动力学导数;等;