Inlets for Supersonic Missiles
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American Institute of Aeronautics and Astronautics, Inc.
Cited by 28 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. Contribution of Different Parameters on Film Cooling Efficiency Based on the Improved Orthogonal Experiment Method;Aerospace;2024-01-10
2. Effects of inflow boundary layer on supersonic inlets;AIAA SCITECH 2024 Forum;2024-01-04
3. Trajectory Analysis of a Solid Fuel Ramjet Propelling an Artillery Shell;Journal of Aerospace Sciences and Technologies;2023-07-30
4. Multi-Objective Optimization of Arbitrary Supersonic Intake Based on Axiomatic Design Theory using Kriging/MOGA;AIAA AVIATION 2023 Forum;2023-06-08
5. Investigation of Flow Phenomena in the Optimization of Supersonic Intake Design with a RANS Solver;25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2023-05-27
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