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2017
8 Citations

Assessment of predictive capabilities for aerodynamic heating in hypersonic flow

Knight, D., Chazot, O., Austin, J., Badr, M. A., Candler, G. V., Celik, B., Rosa, D. D., Donelli, R., Komives, J., Lani, A., Levin, D., Nompelis, I., Panesi, M., Pezzella, G., Reimann, B., Tumuklu, O. & Yuceil, K., Apr 1 2017, In : Progress in Aerospace Sciences. 90, p. 39-53 15 p.

Research output: Contribution to journalReview article

Aerodynamic heating
Hypersonic flow
Hypersonic aerodynamics
Computational fluid dynamics
Plant startup
1 Citations

Characterization of carbon ablation models including effects of gas-phase chemical kinetics

Candler, G. V., Alba, C. R. & Greendyke, R. B., Jan 1 2017, In : Journal of Thermophysics and Heat Transfer. 31, 3, p. 512-526 15 p.

Research output: Contribution to journalArticle

ablation
reaction kinetics
vapor phases
carbon
surface reactions
3 Citations

Computing measured spectra from hypersonic pitot probes with flow-parallel freestream disturbances

Chaudhry, R. S. & Candler, G. V., Jan 1 2017, In : AIAA Journal. 55, 12, p. 4155-4166 12 p.

Research output: Contribution to journalArticle

Parallel flow
Hypersonic aerodynamics
Transfer functions
Direct numerical simulation
Amplification

Coupled conjugate heat transfer simulation for a scramjet inlet at Mach 8

Reinert, J. D., Nompelis, I. & Candler, G. V., Jan 1 2017, 23rd AIAA Computational Fluid Dynamics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Mach number
Heat transfer
Hypersonic inlets
Hypersonic vehicles
Fluids
9 Citations

Direct simulation of hypersonic crossflow instability on an elliptic cone

Dinzl, D. J. & Candler, G. V., Jan 1 2017, In : AIAA Journal. 55, 6, p. 1769-1782 14 p.

Research output: Contribution to journalArticle

Hypersonic aerodynamics
Cones
Surface roughness
Reynolds number
Wavelength

Dynamic mode decomposition of trip-induced hypersonic boundary layer transition

Shrestha, P., Nichols, J. W., Candler, G. V. & Jovanović, M. R., Jan 1 2017, 47th AIAA Fluid Dynamics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Hypersonic boundary layers
Surface roughness
Decomposition
Vortex flow
Flow structure
3 Citations

Finite-rate oxidation model for carbon surfaces from molecular beam experiments

Poovathingal, S., Schwartzentruber, T. E., Murray, V. J., Minton, T. K. & Candler, G. V., Jan 1 2017, In : AIAA Journal. 55, 5, p. 1644-1658 15 p.

Research output: Contribution to journalArticle

Molecular beams
Oxidation
Carbon
Carbon monoxide
Experiments
7 Citations

Global linear stability analysis of high speed flows on compression ramps

Sidharth, G. S., Dwivedi, A., Candler, G. V. & Nichols, J. W., Jan 1 2017, 47th AIAA Fluid Dynamics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Linear stability analysis
Supersonic flow
Navier Stokes equations
Linear systems
Flow fields
2 Citations

Nonequilibrium flow through porous thermal protection materials, Part I: Numerical methods

Stern, E. C., Poovathingal, S., Nompelis, I., Schwartzentruber, T. E. & Candler, G. V., Jan 1 2017, (Accepted/In press) In : Journal of Computational Physics.

Research output: Contribution to journalArticle

nonequilibrium flow
thermal protection
Numerical methods
Ablation
ablation
1 Citations

Numerical simulation of propagation of strong shock waves

Chandel, D., Nompelis, I. & Candler, G. V., Jan 1 2017, AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., AIAA-2017-0744

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shock waves
Shock tubes
Computer simulation
Advection
NASA
2 Citations

Optimal spatial growth of streaks in oblique shock/boundary layer interaction

Dwivedi, A., Nichols, J. W., Jovanovic, M. R. & Candler, G. V., Jan 1 2017, 8th AIAA Theoretical Fluid Mechanics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

boundary layers
Boundary layers
shock
Direct numerical simulation
attachment
3 Citations

Quasiclassical trajectory analysis of N2 + O2 and implications for hypersonic CFD

Chaudhry, R. S., Bender, J. D., Schwartzentruber, T. E. & Candler, G. V., Jan 1 2017, 47th AIAA Thermophysics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Hypersonic aerodynamics
Computational fluid dynamics
Trajectories
Nitrogen
Shock tubes
2 Citations

Scalar conservation and boundedness in simulations of compressible flow

Subbareddy, P. K., Kartha, A. & Candler, G. V., Nov 1 2017, In : Journal of Computational Physics. 348, p. 827-846 20 p.

Research output: Contribution to journalArticle

compressible flow
Compressible flow
conservation
Conservation
Numerical methods

Sensitivity analysis for the control of oblique shock wave/laminar boundary layer interactions at Mach 5.92

Hildebrand, N., Dwivedi, A., Nichols, J. W., Candler, G. V. & Jovanović, M. R., Jan 1 2017, 47th AIAA Fluid Dynamics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Laminar boundary layer
Shock waves
Mach number
Sensitivity analysis
Hypersonic boundary layers
2 Citations

Wall-modeled large-eddy simulation of autoignition-dominated supersonic combustion

Candler, G. V., Cymbalist, N. & Dimotakis, P. E., Jan 1 2017, In : AIAA journal. 55, 7, p. 2410-2423 14 p.

Research output: Contribution to journalArticle

Large eddy simulation
Computational fluid dynamics
Hydrogen
Supersonic flow
Fluid mechanics
2016
3 Citations

Analysis of dissociation and internal energy transfer in high energy N2 + O2 collisions using the quasiclassical trajectory method

Chaudhry, R. S., Bender, J. D., Valentiniy, P., Schwartzentruberz, T. E. & Candler, G. V., Jan 1 2016, 46th AIAA Thermophysics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Energy transfer
Trajectories
Rate constants
Ion exchange
Nitrogen

Application of the evolution-variable manifold approach to cavity-stabilized ethylene combustion

Cymbalist, N., Candler, G. V. & Dimotakis, P. E., Jan 1 2016, 46th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Ethylene
Ignition
Computational fluid dynamics
Large eddy simulation
Combustors
2 Citations

Development and validation of a LES turbulence wall model for compressible flows with heat transfer

Komives, J. R., Subbareddy, P. K. & Candler, G. V., Jan 1 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Compressible flow
Turbulence
Heat transfer
Hypersonic flow
Boundary layers
4 Citations

Direct numerical simulation of crossflow instability excited by microscale roughness on HIFiRE-5

Dinzl, D. J. & Candler, G. V., Jan 1 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Direct numerical simulation
Surface roughness
Coalescence
Mach number
Heat flux
1 Citations

Filtered velocity based LES of mixing in high speed recirculating shear flow

Sidharth, G. S., Kartha, A. & Candler, G. V., Jan 1 2016, 46th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shear flow
Supersonic flow
Hypersonic aerodynamics
Pressure gradient
Compressibility
1 Citations

Finite-rate oxidation model for carbon surfaces from molecular beam experiments

Poovathingal, S., Schwartzentruber, T. E., Murray, V. J., Minton, T. K. & Candler, G. V., Jan 1 2016, 46th AIAA Thermophysics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Molecular beams
Oxidation
Carbon
Experiments
Reaction products
2 Citations

Interaction of an oblique shock with a transitional mach 5.92 boundary layer

Shrestha, P., Dwivedi, A., Hildebrand, N., Nichols, J. W., Jovanovic, M. R. & Candler, G. V., Jan 1 2016, 46th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Direct numerical simulation
Mach number
Boundary layers
Hypersonic boundary layers
Decomposition
1 Citations

Recovery of freestream disturbance spectrum from stagnation pressure spectrum for hypersonic pitot probes

Chaudhry, R. S. & Candler, G. V., Jan 1 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Hypersonic aerodynamics
Transfer functions
Recovery
Pressure transducers
Acoustics

Trip-induced transition of a mach 5.65 low reynolds number boundary layer

Shrestha, P. & Candler, G. V., Jan 1 2016, 46th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Mach number
Wind tunnels
Boundary layers
Reynolds number
Hypersonic aerodynamics
2015
22 Citations

Advances in computational fluid dynamics methods for hypersonic flows

Candler, G. V., Subbareddy, P. K. & Brock, J. M., Jan 1 2015, In : Journal of Spacecraft and Rockets. 52, 1, p. 17-28 12 p.

Research output: Contribution to journalArticle

hypersonic flow
Hypersonic flow
computational fluid dynamics
Computational fluid dynamics
numerical control
13 Citations

Analysis of cross flow instability on HIFiRE-5 using direct numerical simulation

Dinzl, D. J. & Candler, G. V., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-0279

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Direct numerical simulation
Mach number
Tunnels
Vortex flow
Physics
60 Citations
Potential energy surfaces
potential energy
Trajectories
trajectories
dissociation

Calculating high-temperature thermodynamic properties of diatomics in air: Evaluation and accuracy assessment

Daniel Kelley, J., Bender, J. D., Nompelis, I. & Candler, G. V., Jan 1 2015, 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015. AIAA American Institute of Aeronautics and Astronautics

Research output: Chapter in Book/Report/Conference proceedingConference contribution

accuracy assessment
thermodynamic property
Thermodynamic properties
thermodynamic properties
hypersonic flow
4 Citations

Characterization of vibrational and rotational energy transfer in N2 + N2 dissociative collisions using the quasiclassical trajectory method

Bender, J. D., Valentiniy, P., Nompelisz, I., Schwartzentruberx, T. & Candler, G. V., Jan 1 2015, 45th AIAA Thermophysics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-14 14 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Energy transfer
Trajectories
Energy dissipation
Rate constants
Potential energy surfaces
5 Citations

Computational-fluid-dynamics-based axisymmetric aeroshell shape optimization in hypersonic entry conditions

Neville, A. G. & Candler, G. V., Jan 1 2015, In : Journal of Spacecraft and Rockets. 52, 1, p. 76-88 13 p.

Research output: Contribution to journalArticle

aeroshells
shape optimization
hypersonics
Hypersonic aerodynamics
Shape optimization
5 Citations

Detached-eddy simulation of capsule wake flows and comparison to wind-tunnel test data

Schwing, A. M. & Candler, G. V., Jan 1 2015, In : Journal of Spacecraft and Rockets. 52, 2, p. 439-449 11 p.

Research output: Contribution to journalArticle

wind tunnel tests
capsules
wind tunnel
wakes
Wind tunnels
10 Citations

Detached-eddy simulations of hypersonic capsule wake flow

Brock, J. M., Subbareddy, P. K. & Candler, G. V., Jan 1 2015, In : AIAA Journal. 53, 1, p. 70-80 11 p.

Research output: Contribution to journalArticle

Hypersonic aerodynamics
Angle of attack
Mach number
Fluxes
Heat transfer
32 Citations

Development of the US3D code for advanced compressible and reacting flow simulations

Candler, G. V., Johnson, H. B., Nompelis, I., Subbareddy, P. K., Drayna, T. W., Gidzak, V. & Barnhardt, M. D., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-1893

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Flow simulation
NASA
Physics
Hypersonic flow
Fluid structure interaction
35 Citations

Direct molecular simulation of nitrogen dissociation based on an ab initio potential energy surface

Valentini, P., Schwartzentruber, T. E., Bender, J. D., Nompelis, I. & Candler, G. V., Jan 1 2015, In : Physics of Fluids. 27, 8, 1 p.

Research output: Contribution to journalArticle

potential energy
dissociation
nitrogen
simulation
internal energy
2 Citations

Direct numerical simulation of roughness-induced transition in the VKI mach 6 tunnel

Chaudhry, R. S., Subbareddy, P. K., Nompelis, I. & Candler, G. V., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-0274

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Direct numerical simulation
Mach number
Tunnels
Surface roughness
Amplification
6 Citations

Direct simulation of rovibrational excitation and dissociation in molecular nitrogen using an ab initio potential energy surface

Valentini, P., Schwartzentruber, T. E., Bender, J. D., Nompelis, I. & Candler, G. V., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-0474

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Potential energy surfaces
Nitrogen
Trajectories
Electron energy levels
Monte Carlo methods
1 Citations

Large-eddy simulation of autoignition-dominated supersonic combustion

Candler, G. V., Cymbalist, N. & Dimotakis, P. E., Jan 1 2015, 45th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Large eddy simulation
Ignition
Computational fluid dynamics
Convergence of numerical methods
Reaction kinetics
3 Citations

LES of reacting mixing layers: Species concentration boundedness and inflow conditions

Kartha, A., Subbareddy, P. K., Candler, G. V. & Dimotakis, P. E., Jan 1 2015, 22nd AIAA Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fluxes
Temperature
Large eddy simulation
Digital filters
Mach number
3 Citations

Microscale simulations of porous TPS Materials: Ablating microstructures and micro-tomography

Stern, E. C., Nompelis, I., Schwartzentruber, T. E. & Candler, G. V., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-1450

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Tomography
Microstructure
Flow of gases
Porous materials
Chemical reactions
3 Citations

Next-generation CFD for hypersonic and aerothermal flows

Candler, G. V., Jan 1 2015, 22nd AIAA Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Hypersonic aerodynamics
Computational fluid dynamics
Numerical methods
Incompressible flow
Turbulence models
1 Citations

Numerical simulation of surface patterns on sublimating ablative materials

Treviño, L. & Candler, G. V., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-1452

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Ablative materials
Ablation
Reentry
Computer simulation
Numerical methods
19 Citations

Rate-dependent energetic processes in hypersonic flows

Candler, G. V., Jan 1 2015, In : Progress in Aerospace Sciences. 72, p. 37-48 12 p.

Research output: Contribution to journalArticle

Hypersonic flow
Enthalpy
Numerical methods
Direct numerical simulation
Pistons

Stretched-vortex based subgrid-scale modeling for variable-density flows

Sidharth, G. S., Candler, G. V. & Dimotakis, P. E., Jan 1 2015, 45th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Vortex flow
Combustors
Turbulent flow
Large eddy simulation
Vorticity

Thermal non-equilibrium effects in turbulent compressible shear flows

Neville, A. G., Nompelis, I., Subbareddy, P. K. & Candler, G. V., Jan 1 2015, 45th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shear flow
Mach number
Momentum
Computational fluid dynamics
Temperature
2014
6 Citations

Boundary-layer stability analysis of the high enthalpy shock tunnel transition experiments

Gronvall, J. E., Johnson, H. B. & Candler, G. V., Jan 1 2014, In : Journal of Spacecraft and Rockets. 51, 2, p. 455-467 13 p.

Research output: Contribution to journalArticle

boundary layer stability
shock tunnels
enthalpy
stability analysis
Enthalpy

Computational modeling of the flow environment in inductively coupled plasma jet facilities

Norman, P. E., Schwartzentruber, T. E. & Candler, G. V., 2014, 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. American Institute of Aeronautics and Astronautics Inc.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Plasma jets
Inductively coupled plasma
plasma jets
Hypersonic aerodynamics
hypersonics
1 Citations

Computational verification of acoustic damping in high-enthalpy environments

Wagnild, R. & Candler, G. V., Nov 1 2014, In : AIAA journal. 52, 11, p. 2615-2618 4 p.

Research output: Contribution to journalArticle

Enthalpy
Boundary layers
Damping
Acoustics
Laminar boundary layer
27 Citations

Direct numerical simulation of high-speed transition due to an isolated roughness element

Subbareddy, P. K., Bartkowicz, M. D. & Candler, G. V., Jan 1 2014, In : Journal of Fluid Mechanics. 748, 3, p. 848-878 31 p.

Research output: Contribution to journalArticle

Direct numerical simulation
direct numerical simulation
roughness
Surface roughness
high speed

Effect of thermal non-equilibrium on decaying isotropic turbulence

Neville, A. G., Nompelis, I., Subbareddy, P. K. & Candler, G. V., Jan 1 2014, AIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference. American Institute of Aeronautics and Astronautics Inc.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Turbulence
Kinetic energy
Relaxation time
Mach number
Flow fields
2 Citations

Large-eddy simulation of supersonic reacting mixing layers

Kartha, A., Subbareddy, P. K., Candler, G. V. & Dimotakis, P. E., Jan 1 2014, 44th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Large eddy simulation
Limiters
Combustors
Turbulence models
Fluorine