Supersonic Inlet Design using Bleed Boundary Condition with Porosity Variation and Expansion Wave
Author:
Affiliation:
1. Seoul National University
2. Korea Aerospace Industries
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0540
Reference24 articles.
1. Bleed System Design Technology for Supersonic Inlets
2. Flow coefficient behavior for boundary layer bleed holes and slots
3. Flowfield measurements in a normal-hole-bled oblique shock-wave and turbulent boundary-layer interaction
4. Boundary layer development downstream of a bleed mass flow removal region
Cited by 3 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. Parameter Influence on the Porous Bleed Performance with & without Shock-Boundary Layer Interaction;AIAA AVIATION 2022 Forum;2022-06-20
2. Effects of bleed type on the performance of a supersonic intake;Experimental Thermal and Fluid Science;2022-04
3. Supersonic Bleed Rate Model for a Circular Orifice Based on Geometric Similarity;AIAA Journal;2020-06
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