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Start Limits and Positive Control of RBCC Inlet
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2021-11-24 , DOI: 10.1061/(asce)as.1943-5525.0001382 Lei Shi 1 , Yiyan Yang 2 , Xue Yang 2 , Guojun Zhao 2 , Fuhao Chen 2 , Guoqiang He 3
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2021-11-24 , DOI: 10.1061/(asce)as.1943-5525.0001382 Lei Shi 1 , Yiyan Yang 2 , Xue Yang 2 , Guojun Zhao 2 , Fuhao Chen 2 , Guoqiang He 3
Affiliation
A rocket-based combined-cycle (RBCC) inlet is always required to start at a relatively
low Mach number in consideration of the fuel consumption in the ejector mode and the
comprehensive engine performance throughout the flight trajectory. However, ...
中文翻译：
RBCC 入口的起始限制和正控制
考虑到喷射器模式下的燃料消耗和整个飞行轨迹的综合发动机性能，基于火箭的联合循环（RBCC）进气道总是需要在相对较低的马赫数下启动。然而， ...
更新日期：2021-11-24
中文翻译：
RBCC 入口的起始限制和正控制
考虑到喷射器模式下的燃料消耗和整个飞行轨迹的综合发动机性能，基于火箭的联合循环（RBCC）进气道总是需要在相对较低的马赫数下启动。然而， ...
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