The overall layout of rocket-based combined-cycle engines: a review

Author:

Zhang Tian-tianORCID,Wang Zhen-guo,Huang WeiORCID,Chen Jian,Sun Ming-bo

Funder

National Natural Science Foundation of China

the Fund of Outstanding Doctoral Dissertation from the Ministry of Education of China

Publisher

Zhejiang University Press

Subject

General Engineering

Reference106 articles.

1. Anazadehsayed A, Gerdroodbary MB, Amini Y, et al., 2017. Mixing augmentation of transverse hydrogen jet by injection of micro air jets in supersonic crossflow. Acta Astronautica, 137:403–414. https://doi.org/10.1016/j.actaastro.2017.05.007

2. Bian JZ, 2014. Design and Coverage Analysis of Combined Dynamic Space-based Ground-to-ground Combat Aircraft. MS Thesis, Harbin Institute of Technology, Harbin, China (in Chinese).

3. Bond RB, Edwards JR, 2003. CFD analysis of an independently fueled ramjet stream in an RBCC engine. 41st Aerospace Sciences Meeting and Exhibit. https://doi.org/10.2514/6.2003-17

4. Bond RB, Edwards JR, 2004. Computational analysis of an independent ramjet stream in a combined cycle engine. AIAA Journal, 42(11):2276–2283. https://doi.org/10.2514/1.4465

5. Butuk N, Huque Z, Lynch D, 1998. Optimization of an integrated inlet/ejector of an RBCC engine using collaborative optimization. Proceedings of the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Article No. 3567. https://doi.org/10.2514/6.1998-3567

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