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Aerodynamic jet steering using steady blowing and suction

机译:采用稳定的吹气和吸力的气动射流转向

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摘要

An aerodynamic jet steering scheme using a combination of blowing and suction near the exit plane of the primary jet is demonstrated. Previous studies involving synthetic jet actuators have shown that jet steering or vectoring is achieved when primary jet fluid is drawn into the suction slot, and that the vectoring force increases with primary jet speed. These studies were limited by the high-actuation frequencies required to maintain vectoring at high primary jet speeds. The present steady technique does not suffer from this limitation, and requires suction and blowing flow rates which are a small fraction of that of the primary jet. This arrangement is studied experimentally and numerically. The results are presented primarily in terms of turning angle. It is found that for sufficient blowing flow rates (similar to the suction flow rate) the resultant turning angle increases linearly with the suction flow rate regardless of Reynolds number (up to 21,000). For insufficient blowing, the jet may be turned in the opposite direction.
机译:展示了一种在主喷气出口平面附近结合吹风和吸力的气动喷气转向方案。先前涉及合成射流致动器的研究表明,当初级射流流体被吸入吸入槽时,可以实现射流转向或矢量化,并且矢量化力随初级射流速度而增加。这些研究受到在高主喷射速度下保持矢量化所需的高驱动频率的限制。当前的稳定技术不受此限制,并且需要的吸气和吹气流速仅为一次喷射的流速的一小部分。通过实验和数值研究了这种布置。主要以转角表示结果。可以发现,对于足够的吹气流量(与吸气流量相似),无论雷诺数(最大为21,000)如何,最终转向角都会随吸气流量线性增加。对于不充分的吹气,可以将喷头朝相反的方向转动。

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  • 来源
    《Experiments in Fluids》 |2006年第5期|776-785|共10页
  • 作者单位

    Mechanical and Aerospace Engineering Utah State University Logan UT USA;

    Mechanical and Aerospace Engineering Utah State University Logan UT USA;

    Mechanical and Aerospace Engineering Utah State University Logan UT USA;

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  • 原文格式 PDF
  • 正文语种 eng
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