Investigation of Flow Phenomena in the Optimization of Supersonic Intake Design with a RANS Solver-Reference-Cited by-同舟云学术

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Investigation of Flow Phenomena in the Optimization of Supersonic Intake Design with a RANS Solver

Published:2023-05-27 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
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Author:

Singh Sandhu Jatinder Pal¹,Bhardwaj Megha¹,Sharma Anurag¹,Ananthkrishnan N¹,Park Ik-Soo²

Affiliation:

1. Yanxiki Tech

2. Agency for Defense Development

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3019

Reference31 articles.

1. Seddon,J.,andGoldsmith,E.,IntakeAerodynamics,AIAAEducationseries,BlackwellScience,1999.

2. Mahoney,J.J.,InletsforSupersonicMissiles,AIAAEducationSeries,AmericanInstituteofAeronautics&Astronautics,1991. https://doi.org/10.2514/4.403799.

3. Axisymmetric Inlet Design for Combined-Cycle Engines

4. Investigation of Two-Dimensional Scramjet Inlet Flowfield at Mach 7

5. A new approach for the design of hypersonic scramjet inlets

Cited by 1 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. Multi-Objective Optimization of Arbitrary Supersonic Intake Based on Axiomatic Design Theory using Kriging/MOGA;AIAA AVIATION 2023 Forum;2023-06-08

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