Search engine for discovering works of Art, research articles, and books related to Art and Culture
ShareThis
Javascript must be enabled to continue!

Investigations of Trenched Film Hole Orientation Angle on Film Cooling Effectiveness

View through CrossRef
Abstract The effect of altering the orientation angle of trenched film hole on film cooling effectiveness (ƞ) is analyzed through numerical investigation. The film holes were oriented at 6 different angles viz., 0°, 30°, 45°, 90°, 135° and 180° with a fixed inclination angle 30° and with a pitch to diameter (P/D) ratio 5.The length and depth of the trench embedding the film hole are fixed at 3D and 0.75D respectively. Three different blowing ratios M=0.5, 1 and 1.5 were studied. Results from the study reveal that changing the orientation angle of film hole with in trench offered a considerable improvement on ƞ from near film hole region to far downstream location on test surface. For a low blowing ratio of 0.5, the film cooling effectiveness distribution changes with respect to film hole orientation angle and higher ƞ zones are distributed along the corresponding film hole orientation angle. The film hole oriented at 90° with respect to stream wise direction delivered highest ƞ at all three different blowing ratios due to better lateral spreading and uniform coverage of injected coolant. Except near film hole region, 30° and 45° hole orientation produced uniform lateral effectiveness compared to 0° hole orientation.
Title: Investigations of Trenched Film Hole Orientation Angle on Film Cooling Effectiveness
Description:
Abstract The effect of altering the orientation angle of trenched film hole on film cooling effectiveness (ƞ) is analyzed through numerical investigation.
The film holes were oriented at 6 different angles viz.
, 0°, 30°, 45°, 90°, 135° and 180° with a fixed inclination angle 30° and with a pitch to diameter (P/D) ratio 5.
The length and depth of the trench embedding the film hole are fixed at 3D and 0.
75D respectively.
Three different blowing ratios M=0.
5, 1 and 1.
5 were studied.
Results from the study reveal that changing the orientation angle of film hole with in trench offered a considerable improvement on ƞ from near film hole region to far downstream location on test surface.
For a low blowing ratio of 0.
5, the film cooling effectiveness distribution changes with respect to film hole orientation angle and higher ƞ zones are distributed along the corresponding film hole orientation angle.
The film hole oriented at 90° with respect to stream wise direction delivered highest ƞ at all three different blowing ratios due to better lateral spreading and uniform coverage of injected coolant.
Except near film hole region, 30° and 45° hole orientation produced uniform lateral effectiveness compared to 0° hole orientation.

Related Results

Enhancement of Film Cooling Effectiveness Using Dean Vortices
Enhancement of Film Cooling Effectiveness Using Dean Vortices
Abstract Film cooling technology is widely used in gas turbines. Improvement of gas turbine thermal efficiency, specific power and specific thrust can be achieved by...
Numerical Analysis of Film Cooling Performance of Micro Holes and Compound Angle Sister Holes
Numerical Analysis of Film Cooling Performance of Micro Holes and Compound Angle Sister Holes
In the present research, micro holes and compound angle sister holes have been numerically investigated as two different techniques to enhance the cylindrical hole cooling performa...
Numerical Analysis of Film Cooling Performance of Micro Holes and Compound Angle Sister Holes
Numerical Analysis of Film Cooling Performance of Micro Holes and Compound Angle Sister Holes
In the present research, micro holes and compound angle sister holes have been numerically investigated as two different techniques to enhance the cylindrical hole cooling performa...
Large Eddy Simulations on Fan Shaped Film Cooling Hole With Various Inlet Turbulence Generation Methods
Large Eddy Simulations on Fan Shaped Film Cooling Hole With Various Inlet Turbulence Generation Methods
Abstract Large eddy simulations on well-known 7-7-7 fan shaped cooling hole have been carried out. Film cooling methods are generally applied to high pressure turbin...
Application of a CFD-Based Film Cooling Model to a Gas Turbine Vane Cascade With Cylindrical and Shaped Hole Endwall Film Cooling
Application of a CFD-Based Film Cooling Model to a Gas Turbine Vane Cascade With Cylindrical and Shaped Hole Endwall Film Cooling
This paper presents the application of a CFD-based film cooling model to a gas turbine vane cascade test rig. The experimental investigations feature aerodynamic and endwall film c...
Enhancement of Film Cooling Effectiveness Using Dean Vortices
Enhancement of Film Cooling Effectiveness Using Dean Vortices
Abstract Film cooling technology is widely used in gas turbines. With the additive manufacturing anticipated in the future, there will be more freedom in film coolin...
Reclaiming the Wasteland: Samson and Delilah and the Historical Perception and Construction of Indigenous Knowledges in Australian Cinema
Reclaiming the Wasteland: Samson and Delilah and the Historical Perception and Construction of Indigenous Knowledges in Australian Cinema
It was always based on a teenage love story between the two kids. One is a sniffer and one is not. It was designed for Central Australia because we do write these kids off there. N...
Film Cooling of Compound Angle Upstream Sister Holes
Film Cooling of Compound Angle Upstream Sister Holes
Abstract This study introduces a novel and simple strategy; compound angle upstream sister holes (CAUSH) to increase film cooling performance of the cylindrical hole...

Back to Top