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Analysis of thermal ignition in supersonic flat-plate boundary layers
H. G. Im, J. K. Bechtold,
C. K. Law
Mechanical & Aerospace Engineering
High Meadows Environmental Institute
Princeton Institute for the Science and Technology of Materials
Research output
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Contribution to journal
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Article
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peer-review
8
Scopus citations
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Dive into the research topics of 'Analysis of thermal ignition in supersonic flat-plate boundary layers'. Together they form a unique fingerprint.
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Physics & Astronomy
flat plates
100%
ignition
92%
boundary layers
83%
numerical integration
29%
supersonic boundary layers
20%
heating
17%
boundary layer flow
16%
wall temperature
16%
free flow
15%
Mach number
13%
heat transfer
10%
activation energy
10%
interactions
5%
temperature
4%
Engineering & Materials Science
Boundary layers
90%
Ignition
86%
Hot Temperature
46%
Heating
19%
Boundary layer flow
17%
Flow structure
15%
Activation energy
14%
Mach number
13%
Temperature
11%
Heat transfer
9%