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Publications of G. V. Candler


A. Dwivedi,
N. Hildebrand,
J. W. Nichols,
G. V. Candler,
and M. R. Jovanovic.
Transient growth analysis of oblique shock wave/boundarylayer interactions at Mach 5.92.
Phys. Rev. Fluids,
5(6):063904 (20 pages),
June 2020.
Keyword(s): Adjoint equations,
Baseflow sensitivity,
Compressible flows,
Direct numerical simulations,
Energy amplification,
Global stability analysis,
Flow modeling and control,
Hypersonic flows,
Transient growth,
Transition to turbulence.
[bibtexentry]

A. Dwivedi,
G. S. Sidharth,
J. W. Nichols,
G. V. Candler,
and M. R. Jovanovic.
Reattachment vortices in hypersonic compression ramp flow: an inputoutput analysis.
J. Fluid Mech.,
880:113135,
December 2019.
Keyword(s): Compressible flows,
Compression ramp flow,
Flow modeling and control,
Hypersonic flows,
InputOutput analysis,
Shock Boundary layer interaction,
Reattachment vortices,
Transition to turbulence.
[bibtexentry]

N. Hildebrand,
A. Dwivedi,
J. W. Nichols,
M. R. Jovanovic,
and G. V. Candler.
Simulation and stability analysis of oblique shock wave/boundary layer interactions at Mach 5.92.
Phys. Rev. Fluids,
3(1):013906 (23 pages),
January 2018.
Keyword(s): Adjoint equations,
Baseflow sensitivity,
Compressible flows,
Direct numerical simulations,
Global stability analysis,
Flow modeling and control,
Hypersonic flows,
Transition to turbulence.
[bibtexentry]

A. Dwivedi,
G. V. Candler,
and M. R. Jovanovic.
A frequency domain analysis of compressible linearized NavierStokes equations in a hypersonic compression ramp flow.
In Proceedings of the 2020 American Control Conference,
Denver, CO,
pages 43254330,
2020.
Keyword(s): Compressible flows,
Compression ramp flow,
Flow modeling and control,
Hypersonic flows,
InputOutput analysis,
Shock Boundary layer interaction,
Reattachment vortices,
Transition to turbulence.
[bibtexentry]

N. Hildebrand,
A. Dwivedi,
G. S. Sidharth,
J. W. Nichols,
M. R. Jovanovic,
and G. V. Candler.
Instabilities in laminar shock boundary layer interactions.
In Proceedings of the 2019 IUTAM Symposium on LaminarTurbulent Transition,
London, United Kingdom,
2019.
Keyword(s): Adjoint equations,
Baseflow sensitivity,
Compressible flows,
Direct numerical simulations,
Global stability analysis,
Flow modeling and control,
Hypersonic flows,
Transition to turbulence.
[bibtexentry]

A. Dwivedi,
G. S. Sidharth,
G. V. Candler,
J. W. Nichols,
and M. R. Jovanovic.
Inputoutput analysis of shock boundary layer interaction.
In Proceedings of the 48th AIAA Fluid Dynamics Conference,
Atlanta, GA,
pages 3220 (17 pages),
2018.
Keyword(s): Compressible flows,
InputOutput analysis,
Shock Boundary layer interaction,
Hypersonic flows.
[bibtexentry]

N. Hildebrand,
J. W. Nichols,
G. V. Candler,
and M. R. Jovanovic.
Transient growth in oblique shock wave/laminar boundary layer interactions at Mach 5.92.
In Proceedings of the 48th AIAA Fluid Dynamics Conference,
Atlanta, GA,
pages 3221 (17 pages),
2018.
Keyword(s): Adjoints,
Compressible flows,
Global stability analysis,
Hypersonic flows,
Transient growth.
[bibtexentry]

A. Dwivedi,
J. W. Nichols,
M. R. Jovanovic,
and G. V. Candler.
Optimal spatial growth of streaks in oblique shock/boundary layer interaction.
In Proceedings of the 47th AIAA Fluid Dynamics Conference,
Denver, CO,
pages 4163 (17 pages),
2017.
Keyword(s): Compressible flows,
Direct numerical simulations,
Transient growth,
Hypersonic flows,
Transition to turbulence.
[bibtexentry]

N. Hildebrand,
A. Dwivedi,
J. W. Nichols,
G. V. Candler,
and M. R. Jovanovic.
Sensitivity analysis for the control of oblique shock wave/laminar boundary layer interactions at Mach $5.92$.
In Proceedings of the 47th AIAA Fluid Dynamics Conference,
Denver, CO,
pages 4312 (14 pages),
2017.
Keyword(s): Adjoint equations,
Baseflow sensitivity,
Compressible flows,
Direct numerical simulations,
Global stability analysis,
Flow modeling and control,
Hypersonic flows,
Transition to turbulence.
[bibtexentry]

P. Shrestha,
J. W. Nichols,
M. R. Jovanovic,
and G. V. Candler.
Study of tripinduced hypersonic boundary layer transition.
In Proceedings of the 47th AIAA Fluid Dynamics Conference,
Denver, CO,
pages 4513 (21 pages),
2017.
Keyword(s): Direct numerical simulations,
Dynamic mode decomposition,
Roughness elements,
Hypersonic flows,
Transition to turbulence.
[bibtexentry]

P. Shrestha,
A. Dwivedi,
N. Hildebrand,
J. W. Nichols,
M. R. Jovanovic,
and G. V. Candler.
Interaction of an oblique shock with a transitional Mach $5.65$ boundary layer.
In Proceedings of the 46th AIAA Fluid Dynamics Conference,
Washington, DC,
pages 3647 (14 pages),
2016.
Keyword(s): Compressible flows,
Direct numerical simulations,
Dynamic mode decomposition,
Flow modeling and control,
Hypersonic flows,
Transition to turbulence.
[bibtexentry]
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