论文信息 - Low fidelity models applied to the numerical investigation of hypersonic propulsion - 字舞流文

Low fidelity models applied to the numerical investigation of hypersonic propulsion

Carlos R. Ilario da Silva | Mário J. Silva | Ricardo Reis | Pedro M. Goncalves

[1] Juan J. Alonso,et al. SUAVE: An Open-Source Environment for Multi-Fidelity Conceptual Vehicle Design , 2015 .

[2] Juan J. Alonso,et al. SUAVE: An Open-Source Environment for Conceptual Vehicle Design and Optimization , 2016 .

[3] J. A. Roux. Parametric Ideal Scramjet Cycle Analysis , 2011 .