Radiation and roughness effects on the thermochemical erosion of ablative materials in rocket nozzles

Alessandro Turchi, Daniele Bianchi, Piyush Thakre, Francesco Nasuti, Vigor Yang

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

2 Citations (Scopus)

Abstract

Surface roughness and radiative heat transfer effects on the ablative behavior of a graphite nozzle are studied. A validated numerical approach, that relies on a full Navier- Stokes flow solver coupled with a thermochemical ablation model is used for the analysis. A modification of the Spalart-Allmaras turbulence model is implemented to account for surface roughness. Different simplified models are used to evaluate the integral emissivity in case of metallized propellants and the net radiative heat flux is considered in the surface energy balance. Individual and combined effects of these phenomena are analyzed. Results show that the influence of surface roughness and radiation heat transfer on the erosion rate is dependent on the erosion regime.

Original languageEnglish
Title of host publication51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624101816
DOIs
Publication statusPublished - 2013
Event51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013 - Grapevine, TX, United States
Duration: 2013 Jan 72013 Jan 10

Publication series

Name51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013

Other

Other51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013
Country/TerritoryUnited States
CityGrapevine, TX
Period13-01-0713-01-10

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

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