1.

Technical Paper
Technical Paper
1. 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.
Pub. info.: A.S.M.E. paper.  2005.  New York, NY.  American Society of Mechanical Engineers
Title of ser.: ASME Technical Paper : GT
Ser. no.: 2005
2.

Technical Paper
Technical Paper
2. Turbine Blade Platform Film Cooling with Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling.
Gao, Z. ; Narzary, D. ; Han, J-C.
Pub. info.: A.S.M.E. paper.  2008.  New York, NY.  American Society of Mechanical Engineers
Title of ser.: ASME Technical Paper : GT
Ser. no.: 2008
3.

Technical Paper
Technical Paper
3. Effect of Inlet Flow Angle on Gas Turbine Blade Tip Film Cooling.
Gao, Z. ; Narzary, D. ; Mhetras, S. ; Han, J-C.
Pub. info.: A.S.M.E. paper.  2007.  New York, NY.  American Society of Mechanical Engineers
Title of ser.: ASME Technical Paper : GT
Ser. no.: 2007
4.

Technical Paper
Technical Paper
4. 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.
Pub. info.: A.S.M.E. paper.  2007.  New York, NY.  American Society of Mechanical Engineers
Title of ser.: ASME Technical Paper : GT
Ser. no.: 2007