Time-resolved temperature characterization of a hypersonic shock layer using a single high-speed color camera for aerospace design applications
Author:
Funder
Defence Research and Development Organisation
Publisher
IOP Publishing
Subject
Applied Mathematics,Instrumentation,Engineering (miscellaneous)
Link
http://iopscience.iop.org/article/10.1088/1361-6501/ab1c41/pdf
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1. PLANETARY-ENTRY GAS DYNAMICS
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