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Research article

First published 2025-4

Preliminary design of a hypersonic airbreathing vehicle based on four steps: An academic approach to learning

Eduardo Bento Guerra, George Santos Marinho, Douglas do Nascimento Silva [...]

International Journal of Mechanical Engineering Education

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Research article

First published 2019-10

Thrust control strategy based on the minimum combustor inlet Mach number to enhance the overall performance of a scramjet engine

Zifei Ji, Huiqiang Zhang, Bing Wang

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2014-5

Hydrogen-fueled scramjet cooling system investigation using combustor and regenerative cooling coupled model

Wen Bao, Yanjuan Duan, Weixing Zhou

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2016-6

Design methodology for shape transition inlets based on constant contraction of discrete streamtubes

Yabin Xiao, Lianjie Yue, Shenghu Ma [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2024

Numerical investigation on influence of different geometrical cavity flame holders and flame stabilization mechanism in hydrogen fueled multi-strut-based scramjet combustor

Shaik Shajahan, Santhosh Kumar Gugulothu, Raju Muthyala [...]

Proceedings of the Institution of Mechanical Engineers,Part E: Journal of Process Mechanical Engineering

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Research article

First published 2017-2

Surrogate modeling of a 3D scramjet-powered hypersonic vehicle based on screening method IFFD

Chen Boyi, Liu Yanbin, Shen Haidong [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2014-11

Mathematical modeling and characteristic analysis of scramjet buzz

Juntao Chang, Lei Wang, Wen Bao

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2020-5

Combustion efficiency and pressure loss balance for the supersonic combustor

AM Tahsini

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2006-5

Design aspects of launch vehicle sizing including air-breathing propulsion

M Sundaresan

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2005-3

Numerical investigation of transverse sonic injection in a non-reacting supersonic combustor

P Manna, D Chakraborty

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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