Effects of gap leakage on fluid flow in a contoured turbine nozzle guide vane
- Author(s):
- Lin, Y.-L. ( Michigan State University )
- Shih, T.I-P.
- Chyu, M. K.
- Bunker, R. S.
- Publication title:
- A.S.M.E. paper
- Title of ser.:
- ASME Technical Paper : GT
- Ser. no.:
- 2000
- Pub. Year:
- 2000
- No.:
- 2000-GT-555
- Paper no.:
- 2000-GT-555
- Pub. info.:
- New York: American Society of Mechanical Engineers
- Language:
- English
- Call no.:
- A11800
- Type:
- Technical Paper
Similar Items:
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
2
Technical Paper
Measurements of heat transfer characteristics of gap leakage around a misaligned component interface
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Computations of flow and heat transfer in a channel with rows of hemispherical cavities
The American Society of Mechanical Engineers |
10
Technical Paper
Effects of Coating Blockage and Deposit on Film Cooling Effectiveness and Heat Transfer
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
11
Technical Paper
Investigation of the flow field downstream of a turbine trailing edge cooled nozzle guide vane
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |