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Cold flow experimental research of RBCC ejector modal

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TLDR
In this paper, a cold flow experiment was used to investigate the anti-backpressure characteristics of RBCC ejector modal with different configurations, and the results show that the increase of the mixer length can improve the antibackpressure performance, but the performance can not be improved significantly.
Abstract
The method of cold flow experiment was used to research the anti-backpressure characteristics of RBCC ejector modal with different configurationsThe wall surface pressure curve in different length of the mixer and different configurations of main rockets is given by measuring the wall static pressureThe anti-backpressure performances of different configurations are analyzedThe Results show that the increase of the mixer length can improve the anti-backpressure performance,but the performance can not be improved significantly;the double main rockets structure can effectively enhance the anti-backpressure abilityThe test shows that the structure of main rocket has an important influence on anti-backpressure performanceThis test provides a reference for the configuration design of RBCC ejector modal

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Journal ArticleDOI

Survey on key techniques of rocket-based combined-cycle engine in ejector mode

TL;DR: This study aims to provide a summary report on the recent research progress on the RBCC engine in ejector mode from four aspects, namely the combustion organization, the mixing enhancement, the resistance to backpressure and the ejector/ramjet mode transition.
Journal ArticleDOI

Research progress on ejector mode of rocket-based combined-cycle engines

TL;DR: A number of relevant key technologies regarding the study of the ejector mode are proposed, including efficient ejection, efficient mixing and combustion, widely adjustable rocket, widely applicable variable geometry inlet/nozzle design and control, multi-mode flow passage design, and robust mode transition.
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