| 1. | It saves several columns of calculating in the work-up since tunnel wall effect on the horizontal tail is then nonexistent .
因为这时不存在洞壁对平尾的影响，所以数据处理工作量减小了。 |
| 2. | The tail lift curve slope as determined from the panel model may require adjustment in order to apply the test results .
为了应用试验结果，根据翼段模型试验确定的平尾升力曲线斜率可能要作些修正。 |
| 3. | Level - stability - panel is a key component in helicopter
平尾是直升机的重要部件。 |
| 4. | With angels songs , with wild imaginings
平尾昌晃曲 |
| 5. | Firstly , a dynamics equation is got by analyzing the aerodynamics change brought by aircraft differential tail
首先，分析差动平尾所引起的飞机气动力的变化，从而导出相应的飞机动力学方程。 |
| 6. | Finally , the flight control performance is discussed by the aircraft lateral equation of motion when the differential tail works
最后，应用某型飞机的侧向模型，分析差动平尾工作时的控制性能。 |
| 7. | It is one of the important tasks in the design of helicopter to analyze the strength of composite level - stability - panel
某型直升机的平尾是全复合材料结构，对其进行分析是直升机设计中重要工作之一。 |
| 8. | Secondly , the article studies the stability , control performance and reconfiguration ability of the aircraft in theory when the differential tail is used
其次，本文对于差动平尾所引起的飞机稳定性、控制性能的变化及重构能力进行了理论研究。 |
| 9. | The current production rate for boeing 737 ng horizontal stabilizer reached to 17 units per month . the quality of the delivered products met all standard requirements
为美国波音飞机公司生产的波音737ng飞机平尾，已经达到月稳定交付10架的生产能力。 |
| 10. | In this paper , the mechanical character of composite level - stability - panel is analyzed , and the software clop is developed for the analysis of composite laminate strength
论文分析了某型直升机复合材料平尾的力学特性，并开发了能够用于层合结构强度分析的计算机程序。 |
