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Chi-bing Shen

Researcher at National University of Defense Technology

Publications -  32
Citations -  526

Chi-bing Shen is an academic researcher from National University of Defense Technology. The author has contributed to research in topics: Injector & Supersonic speed. The author has an hindex of 11, co-authored 20 publications receiving 317 citations.

Papers
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An overview of waverider design concept in airframe/inlet integration methodology for air-breathing hypersonic vehicles

TL;DR: In this article, the authors reviewed and classified the waverider applications developed by domestic and overseas scholars in the airframe/inlet integration methodology for air-breathing hypersonic vehicles, and the future research and development trends are presented.
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Novel inlet-airframe integration methodology for hypersonic waverider vehicles

TL;DR: In this paper, a novel inlet-airframe integrated axisymmetric basic flow model that accounts for both external and internal flows is first designed using the method of characteristics and the streamline tracing technique.
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An overview of research on waverider design methodology

TL;DR: In this article, the authors present a review and classification of the waverider design methodologies developed by local and foreign scholars up until 2016. The design concept of a WAV can be summarized as follows: modeling of the basic flow field is used to design the WAV in the streamwise direction and the osculating theory is used in the spanwise direction.
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Parametric study on mixing augmentation mechanism induced by cantilevered ramp injectors in a shock-induced combustion ramjet engine

TL;DR: In this article, the studies on standard and swept cantilevered ramp injectors are provided to reveal the mixing enhancement mechanism and the formation of the complex shock wave system, and some parameters are also taken into consideration to evaluate the flow field properties, including the mixing efficiency, the intensity of streamwise vorticity and total pressure recovery efficiency.
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Study on atomization and combustion characteristics of LOX/methane pintle injectors

TL;DR: In this paper, the influence of main structural parameters of the LOX/methane pintle injectors on atomization cone angles and combustion performances were studied by experiments and numerical simulation respectively.