Hybrid Propulsion Parametric and Modular Model: a novel engine analysis tool conceived for design optimization-Reference-Cited by-同舟云学术

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Hybrid Propulsion Parametric and Modular Model: a novel engine analysis tool conceived for design optimization

Published:2014-06-13 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
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Author:

Mogavero Alessandro¹,Taylor Ian¹,Brown Richard E.¹

Affiliation:

1. University of Strathclyde

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2787

Reference16 articles.

1. Scramjet Engines: The First Forty Years

2. SCCREAM (Simulated Combined-Cycle Rocket Engine Analysis Module) - A conceptual RBCC engine design tool

3. Newtonian Flow

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical Modeling and Simulation of Supersonic Flows in Propulsion Systems by Open-Source Solvers;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02

2. An improved engine analysis and optimization tool for hypersonic combined cycle engines;20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2015-07-02

3. Robust Multidisciplinary Design and Optimisation of a Reusable Launch Vehicle;19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2014-06-13

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