航空学报 > 1996, Vol. 17 Issue (1): 18-23

席壁冷却结构的无因次温差比η和θ的实验研究

何立明1, 李长林2, 吴二平2   

  1. 1. 空军工程学院一系,西安, 710038;2. 西北工业大学七研,西安, 710072
  • 收稿日期:1993-12-13 修回日期:1994-10-25 出版日期:1996-02-25 发布日期:1996-02-25

EXPERIMENTAL INVESTIGATIONS ON DIMENSIONLESS TEM PERATURE DIFFERENCE RATIO η AND θ OF MAT-WALL COOLING STRUCTURE

He Liming1, Li Changlin2, Wu Erping2   

  1. 1. Department 7 of Northwestern Polytechnical University, Xi'an, 710072;2. Department 1 of Air For ce Engineering College, Xican, 710038
  • Received:1993-12-13 Revised:1994-10-25 Online:1996-02-25 Published:1996-02-25

摘要: 对席壁冷却结构的平板实验件进行热态实验研究,测定反映该冷却结构冷却效果的两个无因次温差比η和θ的大小随冷却密流man/A平板的变化规律,一方面以检验本席壁结构的冷却效果,另一方面为七热流壁温计算提供支持

关键词: 席壁冷却结构, 无因次温差比, 实验研究, 冷却效果

Abstract: The values of the dimensionless temperature difference ratio η and θ depend on the thermal conductivity of multiple-duct wall,coolant mass flow per unit surface area and geometrical structure of the multiple-hole base.The values of η and θ demonstrate the cooling effect of a cooling structure to a certain extent. Hot state experimental investigation on a piece of experimental plate of mat-wall cooling structure has been done,and the values of η and θ and their variation with the cooling density flow that display the cooling effect of the cooling structure have been determined. The cooling effect of the mat-wall structure can be examined, which can offer support for seven-heat-flow wall temperature calculation.

Key words: mat-wall cooling structure, dimensionless temper ature difference ratio, experimentalinvestigation, cooling effect

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