Author:
Turchi A.,Bianchi D.,Nasuti F.,Onofri M.
Reference28 articles.
1. Effect of pressure and propellant composition on graphite rocket nozzle erosion rate;Acharya;Journal of Propulsion and Power,2007
2. D. Bianchi, F. Nasuti, Thermochemical erosion analysis of carbon–carbon nozzles in solid-propellant rocket motors, in: 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Nashville, TN, July 5–28, 2010, AIAA Paper 2010-7075.
3. Coupled analysis of flow and surface ablation in carbon–carbon rocket nozzles;Bianchi;Journal of Spacecraft and Rockets,2009
4. Thermochemical erosion analysis for graphite/carbon–carbon rocket nozzles;Bianchi;Journal of Propulsion and Power,2011
5. D. Bianchi, F. Nasuti, E. Martelli, M. Onofri, A numerical approach for high-temperatures flows over ablating surface, in: 39th AIAA Thermophysics Conference, Miami, FL, June 25–28, 2007, AIAA Paper 2007-4537.
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