Multidisciplinary Integrated Preliminary Design Applied to Unconventional Aircraft Configurations

著录项

• 来源
  《Journal of Aircraft》 |2008年第2期|共页
• 作者

  Christian Werner-Westphal; Wolfgang Heinze; Peter Horst;

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• 作者单位

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• 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  C_(A/C): = life-cycle costs generated by the aircraft (purchase, depreciation, insurance, spares procurement); C_(CREW): = life-cycle costs of cockpit and cabin crew; C_(FEES): = life-cycle costs of fees and charges; C_(FUEL): = life-cycle costs of fuel; C_(MRO): = life-cycle costs of maintenance, repair, and overhaul; c_(DISP): = specific cost factor for dispatch; c_(LDG): = specific cost factor for landing; c_p: = aerodynamic pressure coefficient; D: = drag force; F~(e): = vector of forces at nodes of finite element; J: = Jacobian matrix; L: = lift force; N: = matrix of form finite element form functions; N_F: = number of total flights during aircraft life cycle; N_(PAX): = number of passenger seats in the aircraft; n~(e): = normal vector of finite element; q: = aerodynamic head; R: =;

  机译：C_（A / C）：=飞机产生的生命周期成本（购买;折旧;保险;备件采购）;C_（CREW）：=座舱和机组人员的生命周期成本;C_（FEES）：=费用的整个生命周期成本;C_（FUEL）：=燃料的生命周期成本;C_（MRO）：=维护;修理和大修的生命周期成本;c_（DISP）：=特定的派遣成本因素;c_（LDG）：=着陆的特定成本因数;c_p：＝空气动力压力系数;D：＝阻力;F〜（e）：=有限元节点上的力矢量;J：=雅可比矩阵;L：=提升力;N：=形式有限元形式函数的矩阵;N_F：=飞机生命周期内的总飞行次数;N_（PAX）：=飞机上的乘客座位数;n〜（e）：=有限元的法向矢量;q：=气动头;R：=;