OPTIMUM CRUISE LIFT COEFFICIENT IN INITIAL DESIGN OF JET AIRCRAFT

被引：12
作者：
MARTINEZVAL, R
PEREZ, E
机构：
[1] Universidad Politecnica de Madrid, Madrid
[2] Department Vehiculos Aeroespaciales, Escuela Tecnica Superior de Ingenieros Aeronauticos, Madrid
来源：
JOURNAL OF AIRCRAFT | 1992年 / 29卷 / 04期
关键词：
D O I：
10.2514/3.46226
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
[No abstract available]
引用
收藏
页码：712 / 714
页数：3
相关论文
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  • [2] Lynch F.T., Commercial Transport-Aerodynamic Design for Cruise Performance Efficiency, AIAA, pp. 81-147, (1982)
  • [3] Roskam J., Airplane Design, (1985)
  • [4] Michaut C., Cavalli D., Huynh H.T., Le Thuy H., Preliminary Design of Civil Transport Aircraft, (1989)
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