Bleed Lip Geometry Effects on the Flow in a Hypersonic Wind Tunnel
Author:
Affiliation:
1. Rutgers University, Piscataway, New Jersey 08854-8058
2. Purdue University, West Lafayette, Indiana 47907-1282
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.23064
Reference11 articles.
1. Fifty years of hypersonics: where we've been, where we're going
2. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
3. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
4. Hypersonic Transition Research in the Boeing/AFOSR Mach-6 Quiet Tunnel
5. Inlet Measurements and Quiet Flow Improvements in the Boeing/AFOSR Mach-6 Quiet Tunnel
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1. Optimization of a Mach-6 Quiet Wind-Tunnel Nozzle;Journal of Spacecraft and Rockets;2018-03
2. Aerothermal characteristics of bleed slot in hypersonic flows;Science China Physics, Mechanics & Astronomy;2015-09-05
3. Development of Aerodynamic Design of Hypersonic Quiet Nozzles;Procedia Engineering;2015
4. Development of Hypersonic Quiet Tunnels;Journal of Spacecraft and Rockets;2008-07
5. Quiet-Flow Ludwieg Tube for Hypersonic Transition Research;AIAA Journal;2008-07
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