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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2001, Vol. 22 ›› Issue (6): 500-504.

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EXPERIMENTAL INVESTIGATION ON FLOW FIELD PROPERTIES AROUND AFT-DECK OF DESTROYER

GU Yun-song, MING Xiao   

  1. Department of Aerodynamics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • Received:2000-11-13 Revised:2001-06-30 Online:2001-12-25 Published:2001-12-25

Abstract:

A seven-hole probe velocity measurement system is developed in this paper, which consists of SHP rake, multi-channel pressure transducers, data acquisition system (16bit A/D) and software. Flow field properties of the aft-deck is studied by making three-dimensional full-scale measurements of a destroyer. The flow field vector maps are given. The results of this study will also provide an experimental datum, from which the safe operating envelope can be worked out; it may also be used to validate computer fluid dynamic predictions.

Key words: sh ip fligh t deck, flow field, full-scale measurement, seven-ho le p robe