Mach 4 Performance of a Hypersonic Streamtraced Inlet - Part 1: Experimental Investigations
Author:
Affiliation:
1. North Carolina State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0065
Reference20 articles.
1. Hypersonic Airbreathing Propulsion
2. Structure of Shock Waves in Cylindrical Ducts
3. Turbulence phenomena in a multiple normal shock wave/turbulent boundary-layer interaction
4. Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow
5. Periodic forcing of a shock train in Mach 2.0 flow
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1. Off-design characteristics of a scoop-type streamline-tracing scramjet inlet;Aerospace Science and Technology;2024-06
2. Experimental Investigations of the Hypersonic Stream-Traced Performance Inlet at Subdesign Mach Number;AIAA Journal;2023-01
3. Experimental Studies of Unstart Shock Dynamics within a Streamtraced Scramjet Inlet;AIAA AVIATION 2022 Forum;2022-06-20
4. Mach 4 Performance of a Hypersonic Streamtraced Inlet – Part 2: Computational Results;AIAA SCITECH 2022 Forum;2022-01-03
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