Author:
Anyoji Masayuki,Okamoto Masato,Fujita Koji,Nagai Hiroki,Oyama Akira
Reference13 articles.
1. Oyama A (2011) Multiobjective design exploration of a Mars Exploration Airplane. Proceedings of 55th Space Sciences and Technology Conference, Japan, p. 1-6.
2. Shigeoka S, Ochi H, Yonemoto K, Kobayashi T, Kato E, et al. (2011) Variable-pressure wind tunnel test on low Reynolds number aerodynamic characteristics of three-dimensional wings. 8th International Conference on Flow Dynamics, Japan.
3. Robert DB, Henry SW, Mark AC, Joel SL, David AS (2006) Design of the ARES mars airplane and mission architecture. J Spacecraft Rockets 43(5): 1026-1034.
4. Mueller TJ, Batill SM (1982) Experimental studies of separation on a two-dimensional airfoil at low Reynolds number. AIAA J 20(4): 457-463.
5. Computational and experimental analysis of a high-performance airfoil under low-Reynolds number flow condition;Anyoji;J Aircraft 51(6),2014
Cited by
13 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献