Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles
Author:
Affiliation:
1. University of Rome “La Sapienza”, 00184 Rome, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.40197
Reference25 articles.
1. A semiquantitative prediction of the erosion of graphite nozzle inserts
2. Erosion of graphite in solid-propellant combustion gases and effects on heat-transfer
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