[American Institute of Aeronautics and Astronautics 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference - Orlando, FL ()] 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference - Finite Element Method for Ablative Thermal Protection Systems Design for Atmospheric Re-Entry Vehicles
Scigliano, Roberto, De Simone, Valeria, De Stefano Fumo, MarioLanguage:
english
DOI:
10.2514/6.2018-5207
File:
PDF, 494 KB
english