Simulation of Liquefying Propellants in Cross-Flow Configurations

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

In this study, the entrainment behavior of paraffin-based hybrid rockets is computationally investigated for varying injection conditions. An axial injection case is presented as a baseline, followed by several cases with varying levels of cross-flow present in the gas-phase flow. Varying the angle of the gas-phase flow is found to have an effect on the droplet generation and entrainment from the paraffin fuel layer. Flow development is found to be similar in most cases, with some anomalous behavior observed during the 45 injection trial. An approach for the quantitative evaluation of droplet entrainment is proposed with the 60 injection angle case found to have the greatest amount of mass entrainment compared to the other cases presented.

Original languageEnglish (US)
Title of host publicationAIAA AVIATION 2022 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106354
DOIs
StatePublished - 2022
EventAIAA AVIATION 2022 Forum - Chicago, United States
Duration: Jun 27 2022Jul 1 2022

Publication series

NameAIAA AVIATION 2022 Forum

Conference

ConferenceAIAA AVIATION 2022 Forum
Country/TerritoryUnited States
CityChicago
Period6/27/227/1/22

All Science Journal Classification (ASJC) codes

  • Energy Engineering and Power Technology
  • Nuclear Energy and Engineering
  • Aerospace Engineering

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