Monte Carlo Analysis of Nonequilibrium Ionized Flows.

Abstract

This final report summarizes the research carried out by our research group concerned with the development of a numerical approach for simulating the flows through and expanding from low-power hydrogen arcjets. In Section 1, we describe the development of a particle-based Monte Carlo approach for simulating the necessary collision and plasma effects that occur in these electric propulsion devices. In Section II, we describe an extensive study to make comparison between our model predictions and existing experimental data. It is concluded that the Monte Carlo approach provides an accurate means for simulating the flow inside of the nozzle of the arcjet offering the potential to improve arcjet performance. It is also concluded that accurate Monte Carlo simulation of the arcjet plumes offers the potential to assess accurately integration of arcjets with real spacecraft geometries.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1996
Accession Number
ADA315593

Entities

People

  • Iain D. Boyd
  • Jitendra Balakrishnan
  • Xiaoming Liu

Organizations

  • Cornell University

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Charged Particles
  • Chemical Kinetics
  • Chemical Reactions
  • Collisions
  • Computational Science
  • Electric Propulsion
  • Energy Transfer
  • Experimental Data
  • Flow Fields
  • Fluid Dynamics
  • Fluid Mechanics
  • Gas Dynamics
  • Materials Processing
  • Monte Carlo Method
  • Simulations
  • Spacecraft

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Plasma Physics.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster