| contributor author | Lucio Torre | |
| contributor author | Angelo Cervone | |
| contributor author | Angelo Pasini | |
| contributor author | Luca d’Agostino | |
| date accessioned | 2017-05-09T00:44:10Z | |
| date available | 2017-05-09T00:44:10Z | |
| date copyright | November, 2011 | |
| date issued | 2011 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-27497#111303_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/146253 | |
| description abstract | The paper shows the results of an experimental campaign conducted in the CPRTF (Cavitating Pump Rotordynamic Test Facility) at ALTA S.p.A., aimed at characterizing the cavitation thermal effects on two tapered-hub, variable-pitch inducers, designated as DAPAMITO. The semiempirical method proposed by Ruggeri and Moore for scaling the thermal cavitation effects has been successfully applied and consequently, a further validation of this method has been provided. The influence of the temperature on the intensity of the performance degradation associated with the attached cavitation instability has been identified as a new typology of cavitation thermal effects. In this case, the inhibition of the bubble growth due to thermal effects can be detected by the reduction of the performance degradation usually associated with this type of instability. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Experimental Characterization of Thermal Cavitation Effects on Space Rocket Axial Inducers | |
| type | Journal Paper | |
| journal volume | 133 | |
| journal issue | 11 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.4005257 | |
| journal fristpage | 111303 | |
| identifier eissn | 1528-901X | |
| keywords | Flow (Dynamics) | |
| keywords | Temperature | |
| keywords | Cavitation | |
| keywords | Temperature effects AND Pumps | |
| tree | Journal of Fluids Engineering:;2011:;volume( 133 ):;issue: 011 | |
| contenttype | Fulltext | |
