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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2018, Vol. 39 ›› Issue (2): 121499-121499.doi: 10.7527/S1000-6893.2017.21499

• Fluid Mechanics and Flight Mechanics • Previous Articles     Next Articles

Application of slotted wall interference assessment and correction technique in transonic wind tunnel

LIU Guangyuan1,2, WEI Zhi2, PENG Xin2, CHEN Dehua1,2, JIA Zhiliang2   

  1. 1. State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, China;
    2. High Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
  • Received:2017-06-12 Revised:2017-10-27 Online:2018-02-15 Published:2018-02-11
  • Supported by:
    State Key Laboratory of Aerodynamics Foundation (SKLA2017-3-2); FengLei Youth Innovation Fund of CARDC (FLYIF20160014)

Abstract: The slotted wall is increasingly adopted in advanced transonic wind tunnels. However, in China, understanding of its interference is relatively limited, and studies on assessment and correction of the interference have not been carried out. In this paper, characteristics of interference of the slotted wall with the standard model of advanced civil configuration are evaluated and corrected based on the homogeneous boundary condition of the ideal slot and the classical method. On the basis of accuracy verification, the difference and regularity of slotted wall interference in ETW and 2.4 m transonic wind tunnels are compared and analyzed. The results show that the corrected data are in good agreement with ETW reference data, and both corrections and interference factors coincide with ETW evaluations. Compared with traditional experimental techniques used for porous walls, the method proposed is clear, simple and fast, and can be conveniently applied to other wind tunnel with similar slotted walls. It can be used as an auxiliary means of wall signature method to improve the quality of domestic experimental data, and can provide reference for the design and debugging of domestic advanced transonic wind tunnels.

Key words: wall interference, ideal slotted wall, homogeneous boundary condition, classical method, standard model test

CLC Number: