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[15] 卫锋, 贺旭照, 贺元元, 等. 三维内转式进气道双激波基准流场的设计方法[J] . 推进技术, 2015, 36(3): 358-364. (WEI Feng, HE Xu-zhao, HE Yuan-yuan, et al. Design Method of Dual-Shock Wave Basic Flow-Field for Inward Turning Inlet[J]. Journal of Propulsion Technology, 2015, 36(3): 358-364.)(编辑:梅瑛) * 收稿日期:2016-05-31;修订日期:2016-07-25。基金项目:国家自然科学基金(51376192;91216303);高超声速冲压发动机技术国防科技重点实验室绵阳分部资助。作者简介:卫锋,男,硕士,研究实习员,研究领域为高超声速飞行器设计。E-mail: wf_nudt@hotmail.com
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