Blank Cover Image

Effect of Inlet Flow Angle on Gas Turbine Blade Tip Film Cooling.

Author(s):
Publication title:
A.S.M.E. paper
Title of ser.:
ASME Technical Paper : GT
Ser. no.:
2007
Pub. Year:
2007
No.:
GT2007-27066
Paper no.:
GT2007-27066
Pages:
11
Pub. info.:
New York, NY: American Society of Mechanical Engineers
Language:
English
Call no.:
A11800
Type:
Technical Paper

Similar Items:

1 Technical Paper Effect of a Cutback Squealer and Cavity Depth on Film-Cooling Effectiveness for a Gas Turbine Blade Tip

S. Mhetras, D. Narzary, Z. Gao, J. Han

American Institute of Aeronautics and Astronautics
7 Technical Paper Film-Cooling Effectiveness on Squealer Rim Walls and Squealer Cavity Floor of a Gas Turbine Blade Tip Using Pressure Sensitive Paint.

Mhetras, S., Yang, H., Gao, Z., Han, J-C.

American Society of Mechanical Engineers
2 Technical Paper Effect of Unsteady Wake on Film-Cooling Effectiveness Distribution on a Gas Turbine Blade with Compound Shaped Holes.

Narzary, D.P., Gao, Z., Mhetras, S., Han, J-C.

American Society of Mechanical Engineers
8 Technical Paper Film-Cooling Effectiveness on a Gas Turbine Blade Tip Using Pressure Sensitive Paint.

Ahn, J., Mhetras, S., Han, J-C.

American Society of Mechanical Engineers
3 Conference Proceedings Effect of Inlet Flow Angle on Gas Turbine Blade Tip Film Cooling

Zhihong Gao, Diganta Narzary, Shantanu Mhetras, Je-Chin Han

American Society of Mechanical Engineers
9 Technical Paper Effect of Unsteady Wake on Full Coverage Film-Cooling Effectiveness for A Gas Turbine Blade

S. Mhetras, J. Han

American Institute of Aeronautics and Astronautics
4 Technical Paper Full Coverage Film Cooling for a Turbine Blade with Axial Shaped Holes

Z. Gao, D. Narzary, S. Mhetras, J. Han

American Institute of Aeronautics and Astronautics
10 Technical Paper Film-Cooling Effectiveness from Shaped Film Cooling Holes for a Gas Turbine Blade.

Mhetras, S., Han, J-C., Rudolph, R.

American Society of Mechanical Engineers
5 Technical Paper Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade.

Mhetras, S., Han, J-C., Rudolph, R.

American Society of Mechanical Engineers
11 Technical Paper Influence of Cooling Flow Rate Variation Gas Turbine Blade Temperature Distributions.

Espionosa, F.Z.S., Han, J.C., Kubiak, J., Narzary, D., Blake, S.

American Society of Mechanical Engineers
6 Technical Paper Turbine Blade Platform Film Cooling with Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling.

Gao, Z., Narzary, D., Han, J-C.

American Society of Mechanical Engineers
12 Conference Proceedings Effect of Unsteady Wake on Film-Cooling Effectiveness Distribution on a Gas Turbine Blade With Compound Shaped Holes

Diganta P. Narzary, Zhihong Gao, Shantanu Mhetras, Je-Chin Han

American Society of Mechanical Engineers
1
 
2
 
3
 
4
 
5
 
6
 
7
 
8
 
9
 
10
 
11
 
12