Title of article :
Discharge Coefficient of 3-in-1 Hole with Various Inclination Angle and Hole Pitch
Author/Authors :
Guangchao، نويسنده , , Li and Huiren، نويسنده , , Zhu and Huiming، نويسنده , , Fan، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2008
Pages :
8
From page :
385
To page :
392
Abstract :
Discharge coefficients of 3-in-1 hole of three inclination angles and three spacing between holes are presented which described the discharge behavior of a row of holes. The inlet and outlet of the 3-in-1 hole both have a 15° lateral expansion. The flow conditions considered are mainstream turbulence intensities and density ratios of secondary flow to mainstream. The momentum flux ratios varied in the range from 1 to 4. The comparison is made of the discharge coefficients of three shaped holes to find an optimal hole with low flow loss. The results show that the discharge coefficients of 3-in-1 hole are highest in three shaped holes and therefore this article is focused on the measurements of discharge coefficients of 3-in-1 hole for various geometries and aerodynamic parameters. The measured results of 3-in-1 hole indicate that turbulence intensities, density ratios and momentum flux ratios have weak influence on discharge coefficients for inclination angle of 20°. The high turbulence intensity yields the small discharge coefficients for inclination angle of 45° and 90°. The increased both momentum flux ratios and density ratios lead to the increased discharge coefficients for inclination angle of 45° and 90°. The increased inclination angle causes the rapidly increased discharge coefficients. There is a weak dependence of discharge coefficients on hole pitches.
Keywords :
Aerospace propulsion system , gas turbine , Discharge coefficient , film cooling hole
Journal title :
Chinese Journal of Aeronautics
Serial Year :
2008
Journal title :
Chinese Journal of Aeronautics
Record number :
2264740
Link To Document :
بازگشت