尾部喷流对飞行器阻力影响的数值模拟分析 / Numerical analysis on effect of engine jet on the aircraft drag
- Resource Type
- Academic Journal
- Source
- 火箭推进 / Journal of Rocket Propulsion. 49(3):105-114
- Subject
底部喷流 双喷管 亚跨超音速 流动干扰 阻力特性 base jet dual nozzle sub-tran-supersonic flow interaction drag increase - Language
- Chinese
- ISSN
- 1672-9374