Inward-Turning Streamline-Traced Supersonic Inlet Design Method for Low-Boom, Low-Drag Applications
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-3700
Reference18 articles.
1. Busemann inlet for hypersonic speeds.
2. Analytical Computation of Leading-Edge Truncation Effects on Inviscid Busemann-Inlet Performance
3. Effect of Truncation on the Performance of Busemann Inlet
4. Design and analysis of streamline traced hypersonic inlets
Cited by 5 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. Direct Measurements of Shock Impingement in a Busemann Inlet via a Miniature Embedded Imaging System;AIAA SCITECH 2023 Forum;2023-01-19
2. Inlet Trade Study for a Low-Boom Aircraft Demonstrator;Journal of Aircraft;2017-07
3. Investigation of Design Method for the Inward Turning Inlet with Controlled Intake Curve;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02
4. Inlet Trade Study for a Low Boom Aircraft Demonstrator;34th AIAA Applied Aerodynamics Conference;2016-06-10
5. SUPIN: A Computational Tool for Supersonic Inlet Design;54th AIAA Aerospace Sciences Meeting;2016-01-02
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