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Acta Aeronautica et Astronautica Sinica ›› 2023, Vol. 44 ›› Issue (16): 127967-127967.doi: 10.7527/S1000-6893.2022.27967

• Fluid Mechanics and Flight Mechanics • Previous Articles     Next Articles

Effects of rectangular pulsed jets on drag and heat reduction of long penetration mode

Xiaodong GUO, Chaoying ZHOU(), Shu’ao WAN   

  1. School of Mechanical and Electrical Engineering,Harbin Institute of Technology (Shenzhen),Shenzhen  518055,China
  • Received:2022-09-05 Revised:2022-09-23 Accepted:2022-11-16 Online:2023-08-25 Published:2022-12-14
  • Contact: Chaoying ZHOU E-mail:cyzhou@hit.edu.cn
  • Supported by:
    Shenzhen Science and Technology Plan Basic Research Project(JCYJ20170307151117299)

Abstract:

As an active drag and heat reduction technology, the counterflowing jet has received extensive attention. However, the bow shock in the long penetration mode of counterflowing jet will oscillate significantly, and the flow field will be extremely unstable. Taking the hemispherical body in hypersonic flow as the research object, the possible suppression or mitigation effect of rectangular pulse jet on long mode flow instability is studied. It is found that compared with the steady jet forming the long penetration mode, the rectangular pulsed jet with different frequencies and amplitudes has an obvious heat reduction effect on the long penetration mode. In addition, while the drag coefficient of the long penetration mode takes the minimum value, the corresponding instantaneous standoff distance does not reach the maximum value, with a certain phase difference between them. The large oscillation of the long penetration mode shock standoff distance formed by the steady jet is clearly suppressed by the rectangular pulsed jet. The research results provide reference for the application and development of the hypersonic rectangular pulsed jet technology.

Key words: hypersonic, rectangular pulsed jet, long penetration mode, unsteady simulation, drag and heat reduction

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