Volume 39 Issue 8
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LIU Runfu, HUANG Yue, LI Zhenyao, et al. Numerical simulation of mixing characteristic of rear variable area bypass injector with lobed structure[J]. Journal of Aerospace Power, 2023, 39(X):20220594 doi: 10.13224/j.cnki.jasp.20220594
Citation: LIU Runfu, HUANG Yue, LI Zhenyao, et al. Numerical simulation of mixing characteristic of rear variable area bypass injector with lobed structure[J]. Journal of Aerospace Power, 2023, 39(X):20220594 doi: 10.13224/j.cnki.jasp.20220594

Numerical simulation of mixing characteristic of rear variable area bypass injector with lobed structure

doi: 10.13224/j.cnki.jasp.20220594
  • Received Date: 2022-08-16
    Available Online: 2023-12-14
  • In order to improve the mixing efficiency of the air flow between the inner and outer bypasses of the rear variable area bypass injector (RVABI) in the variable cycle engine, and to improve the velocity uniformity between the mixed air flows, a method of adjusting the outer bypass area of the RVABI with lobed structure was proposed. By means of numerical simulation, the total pressure loss, thermal mixing efficiency, velocity distribution and vortex evolution were studied and analyzed at the bypass ratio of 0.11−0.23, and the two reference models were compared. The results showed that the method of adjusting the outer bypass area of the variable area bypass injector by introducing the lobed structure can significantly improve the uniformity of the flow field velocity and greatly improve the thermal mixing efficiency of the inner and outer bypasses. And with the increase of the bypass ratio, compared with the reference configuration band, the thermal mixing efficiency of the area adjustment method of the lobed structure was improved more significantly. The mixing degree depended on the scale and influence range of the flow vortex; the lobed shape and corresponding area can be optimized synchronously to further improve the regulating performance.

     

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