skip to main content
OSTI.GOV title logo U.S. Department of Energy
Office of Scientific and Technical Information

Title: Phenomenological and mathematical modeling of a high pressure steam driven jet injector. Part 2

Thesis/Dissertation ·
DOI:https://doi.org/10.2172/80758· OSTI ID:80758
 [1]
  1. The Ohio State Univ., Columbus, OH (United States)

An injector is a particular type of jet pump which uses condensable vapor to entrain a liquid and discharge against a pressure higher than either motive or suction pressures. The injector has no moving parts and requires no external power supply nor any complex control system. Thus, the injector is particularly suited for emergency core cooling operations. A detailed survey has indicated that various injector designs are available for operating pressures below 250 psig. However, the design of these injectors from the viewpoint of a basic understanding of heat and mass transfer processes has not been well developed. A critical review of the models showed serious discrepancies between the analytical models and the experimental observations. The discrepancies evolved from the neglect of non-equilibrium aspects of the flow. The origin of the non-equilibrium aspects can be traced to the extremely small time scales governing the flow in the injector. Thus, time scales of the order of 10-2 seconds are involved in the injector, accompanied by mass, momentum, and heat transfer rates of orders of magnitude higher than that observed in conventional two-phase flows. The present study focuses on the phenomenological and mathematical modeling of the processes in the injector from the viewpoint of its non-equilibrium nature.

Research Organization:
Ohio State Univ. Research Foundation, Columbus, OH (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FG02-88ER12815
OSTI ID:
80758
Report Number(s):
DOE/ER/12815-T1-Pt.2; ON: DE95012601; TRN: 95:016318
Resource Relation:
Other Information: TH: Thesis (Ph.D.); PBD: 1993
Country of Publication:
United States
Language:
English