Type of Document Dissertation Author Reid, Terry Vincent Author's Email Address reid5@prodigy.net URN etd-011099-132537 Title A Computational Approach For Investigating Unsteady Turbine Heat Transfer Due To Shock Wave Impact Degree PhD Department Mechanical Engineering Advisory Committee
Advisor Name Title Wing F. Ng Committee Chair Douglas J. Nelson Committee Member Elaine P. Scott Committee Member Joseph A. Schetz Committee Member Thomas E. Diller Committee Member Keywords
- Unsteady
- computations
- heat flux
Date of Defense 1998-04-30 Availability unrestricted Abstract The effects of shock wave impact on unsteady turbine heat transfer are investigated. A numerical approach is developed to simulate the flow physics present in a previously performed unsteady wind tunnel experiment.The windtunnel experiment included unheated and heated flows over a cascade of highly loaded turbine blades. After the flow over the blades was established, a single shock with a pressure ratio of 1.1 was introduced into the wind tunnel test section. A single blade was equipped with pressure transducers and heat flux microsensors. As the shock wave strikes the blade, time resolved pressure, temperature, and heat transfer data were recorded.
Files
Filename Size Approximate Download Time (Hours:Minutes:Seconds)
28.8 Modem 56K Modem ISDN (64 Kb) ISDN (128 Kb) Higher-speed Access Back.pdf 299.46 Kb 00:01:23 00:00:42 00:00:37 00:00:18 00:00:01 Chapt1.pdf 405.77 Kb 00:01:52 00:00:57 00:00:50 00:00:25 00:00:02 Chapt2.pdf 116.09 Kb 00:00:32 00:00:16 00:00:14 00:00:07 < 00:00:01 Chapt3.pdf 175.48 Kb 00:00:48 00:00:25 00:00:21 00:00:10 < 00:00:01 Chapt4.pdf 165.57 Kb 00:00:45 00:00:23 00:00:20 00:00:10 < 00:00:01 Chapt5.pdf 805.57 Kb 00:03:43 00:01:55 00:01:40 00:00:50 00:00:04 Chapt6.pdf 759.14 Kb 00:03:30 00:01:48 00:01:34 00:00:47 00:00:04 Chapt7.pdf 73.13 Kb 00:00:20 00:00:10 00:00:09 00:00:04 < 00:00:01 Front.pdf 168.93 Kb 00:00:46 00:00:24 00:00:21 00:00:10 < 00:00:01
|
|
If you have questions or technical problems, please Contact DLA.
