| contributor author | H. E. Weber | |
| date accessioned | 2017-05-08T23:38:19Z | |
| date available | 2017-05-08T23:38:19Z | |
| date copyright | October, 1992 | |
| date issued | 1992 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26709#790_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/110186 | |
| description abstract | A method for aerothermodynamic preliminary design of a wave engine is presented. The engine has a centrifugal precompressor for the wave rotor, which feeds high and low-pressure turbines. Three specific wave engine designs are presented. Wave rotor blades are naturally cooled by the ingested air; thus combustion temperatures can be as high as 1900 K. Engine pressure ratios of over 25 are obtained in compact designs. It is shown that placing no nozzles at the end of the rotor blade passages yields the highest cycle efficiencies, which can be over 50 percent. Rotor blades are straight and easily milled, cast, or fabricated. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Wave Engine Aerothermodynamic Design | |
| type | Journal Paper | |
| journal volume | 114 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2906658 | |
| journal fristpage | 790 | |
| journal lastpage | 796 | |
| identifier eissn | 0742-4795 | |
| keywords | Engines | |
| keywords | Waves | |
| keywords | Design | |
| keywords | Rotors | |
| keywords | Blades | |
| keywords | Pressure | |
| keywords | Temperature | |
| keywords | Combustion | |
| keywords | Turbines | |
| keywords | Nozzles | |
| keywords | Cycles AND Engine design | |
| tree | Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 004 | |
| contenttype | Fulltext | |
