Calibration of turbine test rig with impulse turbine at high pressure ratios
The Transonic Turbine Test Rig of the Turbo- Propulsion Laboratory, Department of Aeronautics, of the Naval Postgraduate School was designed to investigate the performance of turbines with transonic or supersonic rotor inlet velocities. The test rig has provisions for testing single stage axial...
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| Language: | en_US |
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Monterey, California. U.S. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/11753 |