Investigation of an Inward Turning Intake in a Mach 6 Quiet Tunnel at Off-Design Conditions
Author:
Affiliation:
1. Purdue University
2. University of Notre Dame
3. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3897
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1. Design concept of three-dimensional section controllable internal waverider hypersonic inlet
2. Design and analysis of streamline traced hypersonic inlets
3. Free-Jet Testing of a REST Scramjet at Off-Design Conditions
4. Waverider Design Methods for Non-Conical Shock Geometries
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