| contributor author | Sumner Alpert | |
| contributor author | R. E. Grey | |
| contributor author | W. O. Flaschar | |
| date accessioned | 2017-05-08T23:25:02Z | |
| date available | 2017-05-08T23:25:02Z | |
| date copyright | January, 1960 | |
| date issued | 1960 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26606#1_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/102612 | |
| description abstract | A three-stage gas turbine was designed to operate at 1750-F inlet temperature with nonstrategic, low alloy components. The rotor blades are cooled with water in a closed system, and the stators are cooled with air. A practical design for the rotor was evolved and tested. Heat-transfer data correlated well with expected values. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Development of a Three-Stage Liquid-Cooled Gas Turbine | |
| type | Journal Paper | |
| journal volume | 82 | |
| journal issue | 1 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3672712 | |
| journal fristpage | 1 | |
| journal lastpage | 9 | |
| identifier eissn | 0742-4795 | |
| keywords | Gas turbines | |
| keywords | Rotors | |
| keywords | Blades | |
| keywords | Stators | |
| keywords | Water | |
| keywords | Temperature | |
| keywords | Heat transfer | |
| keywords | Alloys AND Design | |
| tree | Journal of Engineering for Gas Turbines and Power:;1960:;volume( 082 ):;issue: 001 | |
| contenttype | Fulltext | |
