Highly Compact Supersonic Inlet Design Optimization

Author:

Barr Stephen M.1,O'Gara Michael1,Sinha Neeraj1

Affiliation:

1. Combustion Research and Flow Technology, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 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. Comparative performance analysis of supersonic inlets at various Mach number;1ST INTERNATIONAL CONFERENCE ON ADVANCES IN MATERIAL SCIENCE AND TECHNOLOGY: ICAMST2022;2024

2. Wind Tunnel Test of a Highly-Compact Serpentine Supersonic Inlet;AIAA AVIATION 2022 Forum;2022-06-20

3. Parameterization and optimization design of a two-dimensional axisymmetric hypersonic inlet;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-06-29

4. Design space optimisation of an unmanned aerial vehicle submerged inlet through the formulation of a data-fusion-based hybrid model;The Aeronautical Journal;2021-05-12

5. Large Eddy Simulation of an Optimized Highly-Compact Supersonic Inlet Featuring Internal Compression Spikes;AIAA Scitech 2020 Forum;2020-01-05

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