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Input-output analysis of shock boundary layer interaction
Anubhav Dwivedi
, G. S. Sidharth
,
Graham V. Candler
,
Joseph W. Nichols
, Mihailo R. Jovanović
Aerospace Engineering and Mechanics
Research output
:
Chapter in Book/Report/Conference proceeding
›
Conference contribution
25
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Scopus citations
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Keyphrases
Input-output Analysis
100%
Span-wise
100%
Reattachment
100%
SWBLI
100%
Boundary Layer
66%
Recirculation Bubble
66%
Predictive Control
33%
Frequency Response
33%
Wavelength Selection
33%
Two Dimensional
33%
Receptivity
33%
Asymptotically Stable
33%
Inviscid
33%
Transition Mechanism
33%
Pressure Rise
33%
ReAttach
33%
Steady-state Flow
33%
Boundary Layer Thickness
33%
High-speed Boundary Layer
33%
Optimal Frequency
33%
Aeronautics
33%
Destabilizing Effect
33%
External Perturbation
33%
Bubble Dynamics
33%
Streamwise Vorticity
33%
Compressible Boundary Layer Flow
33%
Double Wedge
33%
Perturbation Growth
33%
Predictive Design
33%
Subwavelength Scale
33%
Engineering
Boundary Layer
100%
Layer Interaction
100%
Reattachment
42%
Layer Flow
14%
Two Dimensional
14%
Aviation
14%
Streamlines
14%
Pressure Rise
14%
Steady State Flow
14%
Optimal Frequency
14%
Boundary Layer Thickness
14%
Frequency Response
14%
Streamwise Vorticity
14%
Earth and Planetary Sciences
Input-Output Analysis
100%
Boundary Layer
100%
Boundary Layer Thickness
16%
Compressible Boundary Layer
16%
Boundary Layer Flow
16%