Highly Compact Supersonic Inlet Design Optimization
Author:
Affiliation:
1. Combustion Research and Flow Technology, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4842
Reference17 articles.
1. Design and Analysis Tool for External-Compression Supersonic Inlets
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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
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