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- pulse combustion wind tunnel 脉冲式燃烧风洞
- Impulse combustion wind tunnel and its application in rocket and scramjet research 脉冲燃烧风洞及其在火箭和超燃发动机研究中的应用
- combustion wind tunnel 燃烧风洞
- The planes survived the wind tunnel test intact. 这些纸飞机在测试风道中丝毫未损。
- It is not correct to think of the wind tunnel having uniform flow. 设想风洞具有均匀的气流是不正确的。
- The understanding to the driven mechanism of pulse combustion is key point in researching and devoloping of pulse combustion burner. 对脉冲燃烧的驱动机理的理解和认识是实用脉冲燃烧器研究与开发的关键。
- Setting very low speeds in a wind tunnel is always a vexatious problem. 在风洞中调出低风速来始终是一个麻烦问题。
- In this paper, the advances in research on pulse combustion drying were reviewed and the various forms of dryer with pulse combustor were introduced and discussed. 脉动燃烧干燥是一种新型、高效干燥技术，是利用脉动燃烧产生的高温、高速振荡气流对物料进行干燥的。
- It should be noted that a balance is not always required in a wind tunnel. 应该指出，天平对风洞来说并非是绝对必须的。
- The aerodynamics characteristics of this airfoil is studied in wind tunnel. 进行了翼型的低速气动力性能研究，为附面层特性研究提供了方向。 结果表明，该翼型具有较好的升阻和俯仰特性，但失速特性差。
- The wind tunnel is produced under a technical cooperation agreement with Ford Co of US. 风洞机是根据与美国福特公司的技术合作协议生产的。
- Any flight test and wind tunnel correlation always suffers from a great number of unknowns. 在对飞行试验与风洞试验进行比较时总有大量的未知数。
- ANALYSIS OF IGNITION IN PULSE COMBUSTION 脉冲燃烧着火过程分析
- The experiments were conducted in a wind tunnel at a location 50 ft downwind from the fan. 实验是在风洞中距离风机50英尺处进行。
- Advances in Pulse Combustion Drying 脉动燃烧干燥技术研究进展
- The damping derivatives can only be determined experimentally in the wind tunnel or ballistic range. 阻尼导数只能用风洞或弹道试验来确定。
- digital pulse combustion control 数字化脉冲燃烧控制
- In the experiment under the 20 m/s wind tunnel conditions, the wind abrasion modulus is almost zero. 在每秒20米的风洞实验中，吹蚀模数几乎为零。
- In this paper, the initial stage in application of fuzzy logic to aircraft high-angle-of attack aerodynamics using wind tunnel test data is outlined. 本文概述最初阶段利用风洞试验数据应用模糊逻辑研究飞机大攻角空气动力学的情况。
- In the experiment under the 20 m/s wind tunnel conditions,the wind abrasion modulus is almost zero. 在每秒20米的风洞实验中，吹蚀模数几乎为零。
