| タイトル | Sensing and actuation in a liquid propellant rocket engine |
| 著者（英） | Bentsman, Joseph; Pearlstein, Arne J.; Wilcutts, Mark |
| 著者所属（英） | NASA |
| 発行日 | 1991-01-01 |
| 言語 | eng |
| 内容記述 | Equations describing the conservation of mass, momentum, and energy, and multicomponent transport and chemical reaction in a liquid propellant rocket (LPR) engine are given, along with appropriate boundary conditions. The formulation includes a detailed description of the two-phase (gas/liquid) flow in terms of a moving boundary problem, with droplets and vapor occupying time-dependent subdomains of the LPR chamber. Several sensor and actuator types are considered in detail, and their mathematical descriptions are incorporated into the differential equations and boundary conditions. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 92A29354 |
| 権利 | Copyright |
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