| 航路爬升性能计算 |
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| 引用本文： | 傅职忠.航路爬升性能计算[J].中国民航学院学报,1991(2). |
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| 作者姓名： | 傅职忠 |
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| 作者单位： | 中国民航学院航行系 |
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| 摘 要： | 本文以 B737—300为例介绍了根据飞机及发动机的极曲线、最大爬升推力和燃油流量等原始数据及给定的爬升规律(如表速250KT/280KT/M0.74)计算在标准大气和非标准大气中航路爬升性能的方法及程序,计算结果与该机型使用手册中给出的 ISA—10,ISA,…,ISA 20的爬升数值表非常吻合。本文所述的方法及程序是通用的,对大爬升角的情况亦适用。
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| 关 键 词： | 飞行性能 航路爬升 性能计算 |
Calculation of Enroute Climb Performance |
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| Fu Zhizhong.Calculation of Enroute Climb Performance[J].Journal of Civil Aviation University of China,1991(2). |
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| Authors: | Fu Zhizhong |
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| Institution: | Civil Aviation Institute of China |
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| Abstract: | This paper presents a method and a computer program of calculating enroute climb perfomance in standard and nonstandard atmosphere by using the data of airplane po- lar curve,engine max.climb thrust and fuel flow,according to the given climb rule (for exam- ple,250kt/280kt/M0.74).As an example,the B737-300 (CFM56-3B1) enroute climb per- formance is calculated and the results obtained exactly agree with the climb data tables for ISA-10,ISA,...,ISA 20 given in the airplane OPERATIONS MANUAL.The mehtod and program are in general use and are also applicable to calculating enroute steep climbing. |
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| Keywords: | flight performance enroute climb performance calculation |
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