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High-speed shock-boundary-layer interaction over deformed surfaces
Ioannis W. Kokkinakis
,
Dimitris Drikakis
, S. Michael Spottswood
, Kirk R. Brouwer
, Zachary B. Riley
Institute for Advanced Modeling and Simulation
Air Force Research Laboratory
Research output
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peer-review
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Keyphrases
Shock Wave Boundary Layer Interaction
100%
Span-wise
100%
Deformable Surface
100%
Mean Pressure
75%
Deformation Amplitude
75%
Deformation Mode
50%
Surface Deformation
50%
High-order
25%
Numerical Simulation
25%
Contour Plots
25%
Root Mean Square
25%
Supersonic Turbulent Boundary Layer
25%
Oblique Shock
25%
Streamwise
25%
Turbulent Boundary Layers
25%
Boundary Layer Thickness
25%
Turbulent Layers
25%
Reynolds Stress Anisotropy
25%
Panel Buckling
25%
Surface Contour
25%
Surface Curvature
25%
Maximum Deformation
25%
Deformation Rate
25%
Pressure Amplitude
25%
Turbulent Velocity Fluctuations
25%
Two-dimensional Surface
25%
Interaction Buckling
25%
Pressure Surface
25%
Thin Panel
25%
Pressure Forming
25%
Engineering
Boundary Layer
100%
Layer Interaction
100%
Turbulent Boundary Layer
50%
Deformation Mode
50%
Spanwise Distribution
50%
Surface Deformation
50%
Two Dimensional
25%
Reynolds Stress
25%
Contour Plot
25%
Oblique Shock
25%
Streamwise
25%
Boundary Layer Thickness
25%
Root Mean Square
25%
Rate Deformation
25%
Dimensional Surface
25%
Pressure Surface
25%
Pressure Amplitude
25%
Square Pressure
25%
Forming
25%
Turbulent Velocity Fluctuation
25%
Computer Simulation
25%