| 飞机失速/螺旋模型自由飞试验总体方案构想中几个问题的分析 |
| |
| 引用本文： | 许光明,旷天金,欧阳凯. 飞机失速/螺旋模型自由飞试验总体方案构想中几个问题的分析[J]. 实验流体力学, 1990, 0(2) |
| |
| 作者姓名： | 许光明 旷天金 欧阳凯 |
| |
| 作者单位： | 中国空气动力研究与发展中心(许光明，旷天金)，中国空气动力研究与发展中心(欧阳凯) |
| |
| 摘 要： | 本文对制定飞机失速/螺旋模型自由飞试验总体方案时必然会遇到的一些重要问题进行了分析,其内容涉及模型缩尺比例数 K 的最佳选取、确定飞机进入螺旋特征模拟高度 H_A 的依据、模型投放高度 H_m 的变化范围和试验模型质量 M_m 的控制问题。本文所作的各种分析和提出的原则对各种模型自由飞失速/螺旋试验研究具有普遍意义。
|
| 关 键 词： | 失速/螺旋模型自由飞试验 模型缩尺比例数 飞机进入螺旋的特征高度 模型投放高度 模型质量 |
ANALYSES OF SOME PROBLEMS IN OVERALL CONCEPTION OF AIRCRAFT STALL/SPIN MODEL FREE FLIGHT TEST |
| |
| Xu Guangming,Kuang Tianjin,Ouyang Kai. ANALYSES OF SOME PROBLEMS IN OVERALL CONCEPTION OF AIRCRAFT STALL/SPIN MODEL FREE FLIGHT TEST[J]. Experiments and Measur in Fluid Mechanics, 1990, 0(2) |
| |
| Authors: | Xu Guangming Kuang Tianjin Ouyang Kai |
| |
| Affiliation: | China Aerodynamics Research and Development Center |
| |
| Abstract: | Some important problems that are inevitably encountered in overall Conception of airCraft stall/spin model free flight testsare analysed.Included are the optimal selection of model scale,thebasis for determining the CharaCteristiC simulation altitude that air-Craft enters a spin,the range of the altitude to drop model and the Control of the model mass.The analyses and prinCiples made herein are of uniVersal signifi-cance for the stall/spin research of Various model free flight tests. |
| |
| Keywords: | stall/spin model free flight test model scale characteristic altitude of aircraft entering a spin altitude of dropping model model mass |
| 本文献已被 CNKI 等数据库收录！ |
