HIFiRE-5 Boundary-Layer Transition Measured in a Mach-6 Quiet Tunnel with Infrared Thermography
Author:
Affiliation:
1. University of Notre Dame, Notre Dame, Indiana 46556
2. University of Maryland, College Park, Maryland 20742
3. U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433-7542
Funder
National Defense Science and Engineering Graduate Fellowship
Summer Faculty Fellowship Program
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056750
Reference66 articles.
1. Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes
2. Aerodynamic Noise in Supersonic Wind Tunnels
3. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
4. Hypersonic International Flight Research and Experimentation (HIFiRE) Fundamental Science and Technology Development Strategy
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