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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2009, Vol. 30 ›› Issue (10): 1809-1815.

• 流体力学、飞行力学与发动机 • Previous Articles     Next Articles

Heat Transfer Measurements on a Rotating Film Cooling Model

Yang Bin1, Xu Guoqiang2, Wu Hongwei2   

  1. 1 Center of Aviation Safety Technology, Civil Aviation Administration of China2 School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
  • Received:2008-07-29 Revised:2008-10-18 Online:2009-10-25 Published:2009-10-25
  • Contact: Yang Bin

Abstract: An experimental study is performed to investigate the local heat transfer coefficient distribution on a flat blade model under rotating operating conditions. The steady-state thermochromic liquid crystal (TLC) technique is employed to measure the two-dimensional surface temperature, and all the signals from the rotating reference frame are collected and transmitted to the stationary receiver by a telemetering instrument via a wireless connection. During the experiment, both air and CO2 are used as coolants. Detailed distributions of h/h0, which is the ratio of heat transfer coefficient with film cooling to that without, are presented at various mainstream Reynolds numbers (ReD) and rotation numbers (Rt). Results show that the rotational effect has a significant influence on heat transfer coefficient distribution. The profiles of h/h0 deflect towards high-radius locations both on the pressure surface and suction surface, and the deflective tendency of h/h0 is more evident on the suction surface. All the values of h/h0 enhance with increased ReD on the pressure surface, while the distribution of h/h0 declines at first but then augments again on the suction surface. Furthermore, the variation of ReD has little influence on the deflective profiles of h/h0.

Key words: film cooling, heat transfer, flat blade, thermochromic liquid crystal, rotation

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