Experimental investigation of double rows film cooling on vane pressure side

T. Elnady, Ibrahim Hassan, L. Kadem, T. Lucas

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

An experimental investigation has been performed to study the effect of hole shape and position on the cooling performance of a gas turbine stator. Two rows of laid-back fanshaped holes are placed on the pressure side of a scaled vane in a two-dimensional cascade and compared with two identical rows of standard cylindrical exit. Both hole shapes have the same base diameter and were investigated at three different blowing ratios (1, 1.35, and 1.7) with the same coolant flow rate used in each case. The experiments are conducted for the first row of holes only, then for the second row only, and finally for both two rows together at a 0.9 density ratio. The mainstream inlet Reynolds number based on the true chord is 1.4E5 and the exit Mach number is 0.23. The local distributions of the heat transfer coefficient and film cooling effectiveness are obtained using a transient TLC technique. The second row of holes, with by a higher local radius of curvature, shows a 40% decrease in the cooling effectiveness as well as a 10% increase in the heat transfer coefficient near downstream of the hole compared with that obtained by the first hole. The double injection provides a slight increase in the cooling effectiveness and a lower heat transfer coefficient due to the favorable interaction between both injections.

Original languageEnglish
Title of host publicationASME 2012 International Mechanical Engineering Congress and Exposition, IMECE 2012
Pages1917-1926
Number of pages10
Volume7
EditionPARTS A, B, C, D
DOIs
Publication statusPublished - 2012
Externally publishedYes
EventASME 2012 International Mechanical Engineering Congress and Exposition, IMECE 2012 - Houston, TX, United States
Duration: 9 Nov 201215 Nov 2012

Other

OtherASME 2012 International Mechanical Engineering Congress and Exposition, IMECE 2012
CountryUnited States
CityHouston, TX
Period9/11/1215/11/12

Fingerprint

Heat transfer coefficients
Cooling
Blow molding
Coolants
Stators
Mach number
Gas turbines
Reynolds number
Flow rate
Experiments

ASJC Scopus subject areas

  • Mechanical Engineering

Cite this

Elnady, T., Hassan, I., Kadem, L., & Lucas, T. (2012). Experimental investigation of double rows film cooling on vane pressure side. In ASME 2012 International Mechanical Engineering Congress and Exposition, IMECE 2012 (PARTS A, B, C, D ed., Vol. 7, pp. 1917-1926) https://doi.org/10.1115/IMECE2012-85875

Experimental investigation of double rows film cooling on vane pressure side. / Elnady, T.; Hassan, Ibrahim; Kadem, L.; Lucas, T.

ASME 2012 International Mechanical Engineering Congress and Exposition, IMECE 2012. Vol. 7 PARTS A, B, C, D. ed. 2012. p. 1917-1926.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Elnady, T, Hassan, I, Kadem, L & Lucas, T 2012, Experimental investigation of double rows film cooling on vane pressure side. in ASME 2012 International Mechanical Engineering Congress and Exposition, IMECE 2012. PARTS A, B, C, D edn, vol. 7, pp. 1917-1926, ASME 2012 International Mechanical Engineering Congress and Exposition, IMECE 2012, Houston, TX, United States, 9/11/12. https://doi.org/10.1115/IMECE2012-85875
Elnady T, Hassan I, Kadem L, Lucas T. Experimental investigation of double rows film cooling on vane pressure side. In ASME 2012 International Mechanical Engineering Congress and Exposition, IMECE 2012. PARTS A, B, C, D ed. Vol. 7. 2012. p. 1917-1926 https://doi.org/10.1115/IMECE2012-85875
Elnady, T. ; Hassan, Ibrahim ; Kadem, L. ; Lucas, T. / Experimental investigation of double rows film cooling on vane pressure side. ASME 2012 International Mechanical Engineering Congress and Exposition, IMECE 2012. Vol. 7 PARTS A, B, C, D. ed. 2012. pp. 1917-1926
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