Quantification of Supersonic Impulse Flow Conditions via High-Bandwidth Wavelength Modulation Absorption Spectroscopy
Author:
Affiliation:
1. Department of Mechanical Engineering, Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053842
Reference22 articles.
1. Design and Characterization of the Stanford 6 Inch Expansion Tube
2. Development of a Model Scramjet Combustor
3. Ignition and Flame Structure in a Compact Inlet/Scramjet Combustor Model
4. Combustion characteristics of an inlet/supersonic combustor model
5. Test flow disturbances in an expansion tube
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