| contributor author | R. H. Fashbaugh | |
| contributor author | V. L. Streeter | |
| date accessioned | 2017-05-08T23:32:16Z | |
| date available | 2017-05-08T23:32:16Z | |
| date copyright | December, 1965 | |
| date issued | 1965 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-27267#1011_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/106723 | |
| description abstract | A transient flow analysis of a longitudinal vibration in a liquid rocket engine propellent feed system and its supporting structural framework is described, together with supporting experimental tests. Nonlinear friction losses are used in the partial differential equations of continuity and momentum describing the unsteady flow. These equations are solved by the methods of characteristics and placed in form suitable for digital computation. The turbopump steady-state characteristic curves are used to find the transient pressure rise across the pump, and the effects of pump inlet cavitation are estimated from experimental data. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Resonance in Liquid Rocket Engine Systems | |
| type | Journal Paper | |
| journal volume | 87 | |
| journal issue | 4 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3650792 | |
| journal fristpage | 1011 | |
| journal lastpage | 1017 | |
| identifier eissn | 1528-901X | |
| keywords | Resonance | |
| keywords | Rocket engines | |
| keywords | Pumps | |
| keywords | Vibration | |
| keywords | Computation | |
| keywords | Equations | |
| keywords | Partial differential equations | |
| keywords | Pressure | |
| keywords | Momentum | |
| keywords | Flow (Dynamics) | |
| keywords | Friction | |
| keywords | Cavitation | |
| keywords | Steady state AND Unsteady flow | |
| tree | Journal of Fluids Engineering:;1965:;volume( 087 ):;issue: 004 | |
| contenttype | Fulltext | |