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XU B B,LIU T S,WU C J,et al. Research of the continuous scan test method for inlet in low wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2022,36(X):1-10. doi: 10.11729/syltlx20220032
Citation: XU B B,LIU T S,WU C J,et al. Research of the continuous scan test method for inlet in low wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2022,36(X):1-10. doi: 10.11729/syltlx20220032

Research of the continuous scan test method for inlet in low wind tunnel

doi: 10.11729/syltlx20220032
  • Received Date: 2022-04-20
  • Accepted Date: 2022-06-20
  • Rev Recd Date: 2022-05-24
  • Available Online: 2022-10-09
  • The continuous scan test method for the inlet of airplane was studied in the FL–13 wind tunnel of CARDC. The test methods and procedures were proposed and the test data processing methods were also provided. Inlet tests were performed in the FL–13 wind tunnel to compare the conventional test method with the continuous scan test method. The test results with the continuous scan test method have a good consistency with the conventional test method, which verifies the availability and feasibility of the continuous scan test method for the inlet in the low speed wind tunnel. The research results show that the continuous scan test method can raise the tests efficiency and acquire more test data for the inlet test in the wind tunnel.
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