Glow Discharge-Tracer Technique for Velocity Profile Measurement in Hypersonic Boundary Layer Flows
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/53/615/53_615_154/_pdf
Reference17 articles.
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2. Reynolds Number Effects on Shock-Wave Turbulent Boundary-Layer Interactions
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4. Progress in laser spectroscopic techniques for aerodynamic measurements - An overview
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