Freestream Effects on Boundary Layer Disturbances for HIFiRE-5
Author:
Affiliation:
1. Air Force Research Laboratory
2. Texas A&M University
3. United States Air Force
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0278
Reference33 articles.
1. Hypersonic International Flight Research and Experimentation (HIFiRE) Fundamental Science and Technology Development Strategy
2. Hypersonic International Flight Research and Experimentation Technology Development and Flight Certification Strategy
3. Analysis of Crossflow Transition Flight Experiment aboard Pegasus Launch Vehicle (Invited)
4. Crossflow disturbances in three-dimensional boundary layers: nonlinear development, wave interaction and secondary instability
5. Crossflow Instabilities - Theory & Technology
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