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Aero-thermal decomposition of hypersonic boundary layer over blunt cone
Mary L. Houston
, David A. Cook
,
Joseph W. Nichols
Aerospace Engineering and Mechanics
Research output
:
Chapter in Book/Report/Conference proceeding
›
Conference contribution
1
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Scopus citations
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Dive into the research topics of 'Aero-thermal decomposition of hypersonic boundary layer over blunt cone'. Together they form a unique fingerprint.
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Keyphrases
Hypersonic Boundary Layer
100%
Thermal Decomposition
100%
Aero-thermal
100%
Blunt Cone
100%
Boundary Layer
66%
Fluid Thermodynamics
66%
Output Response
50%
Layer Edge
50%
Input-output Analysis
33%
Flat Plate
33%
Streamwise
33%
Second Mode
33%
Inflection Point
33%
Acoustic Component
33%
Input Sensitivity
33%
Direct numerical Simulation
16%
Laminar-turbulent Transition
16%
Input-output
16%
Complex Flow
16%
Surface Roughness
16%
Local Minima
16%
Normal Response
16%
Linear Stability Theory
16%
Slowly Varying
16%
Flow Physics
16%
Eigenfunctions
16%
Thermal Component
16%
Sensitivity Response
16%
Cone Geometry
16%
Parallel Flow
16%
Parabolized Stability Equations
16%
Sharp Cone
16%
Three-fluid
16%
Entropy Layer
16%
Nose Bluntness
16%
Critical Layers
16%
Varying Boundary
16%
Momentum Potential Theory
16%
Output Amplitude
16%
Thermodynamic Component
16%
Thermodynamic Structure
16%
Relative Output
16%
Engineering
Boundary Layer
100%
Output Response
50%
Streamwise
33%
Inflection Point
33%
Input Sensitivity
33%
Flat Plate
33%
Reference Case
16%
Flow Physic
16%
Output Result
16%
Linearized Stability
16%
Local Minimum
16%
Eigenvector
16%
Parallel Flow
16%
Output Amplitude
16%
Direct Numerical Simulation
16%