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  • 2020
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  • Graham V Candler
2019

Verification of a conjugate heat transfer tool with us3d

Reinert, J. D., Dwivedi, A. & Candler, G. V., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

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

Input-output analysis of entropy layer instability on a 35o ogive geometry

Barrett, A. N., Cook, D. A., Thome, J., Nichols, J. W. & Candler, G. V., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

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

2017

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

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

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

2 Scopus citations
2018

Numerical study of trip spacing in hypersonic boundary layer transition

Shrestha, P. & Candler, G. V., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

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

1 Scopus citations

Computations of high enthalpy shock propagation in electric arc shock tube (EAST) at NASA ames

Chandel, D., Nompelis, I. & Candler, G. V., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

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

1 Scopus citations
2017

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, (47th AIAA Fluid Dynamics Conference, 2017).

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

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, (47th AIAA Thermophysics Conference, 2017).

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

5 Scopus citations
2019

Simulating schlieren and shadowgraph images from LES data

Luthman, E., Cymbalist, N., Lang, D., Candler, G. & Dimotakis, P., Aug 1 2019, In : Experiments in Fluids. 60, 8, 134.

Research output: Contribution to journalArticle

Open Access
1 Scopus citations

Rate Effects in Hypersonic Flows

Candler, G. V., Jan 5 2019, In : Annual Review of Fluid Mechanics. 51, p. 379-402 24 p.

Research output: Contribution to journalReview article

7 Scopus citations
2018

An improved ducros sensor for the simulation of compressible flows with shocks

Hendrickson, T. A., Kartha, A. & Candler, G. V., 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3710. (2018 Fluid Dynamics Conference).

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

1 Scopus citations

Quasiclassical trajectory analysis of nitrogen for high-temperature chemical kinetics

Chaudhry, R. S., Bender, J. D., Schwartzentruber, T. E. & Candler, G. V., 2018, In : Journal of thermophysics and heat transfer. 32, 4, p. 833-845 13 p.

Research output: Contribution to journalArticle

6 Scopus citations
2019

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

Stern, E. C., Poovathingal, S., Nompelis, I., Schwartzentruber, T. E. & Candler, G. V., Mar 1 2019, In : Journal of Computational Physics. 380, p. 408-426 19 p.

Research output: Contribution to journalArticle

4 Scopus citations
2017

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

Open Access
4 Scopus 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

12 Scopus citations
2018

Direct numerical simulation of BOLT hypersonic flight vehicle

Thome, J., Dwivedi, A., Nichols, J. W. & Candler, G. V., 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-2894. (2018 Fluid Dynamics Conference).

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

4 Scopus citations
2020

LES of Subsonic Reacting Mixing Layers

Kartha, A., Subbareddy, P. K. & Candler, G. V., Apr 1 2020, In : Flow, Turbulence and Combustion. 104, 4, p. 947-976 30 p.

Research output: Contribution to journalArticle

2018

Effects of variable wall temperature distributions on 3D boundary layers

Thome, J., Reinert, J. D., Dwivedi, A. & Candler, G. V., 2018, 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-5271. (22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference).

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

Computational study of high speed flow on a sliced cone-flap geometry

Thome, J., Reinert, J. D., Dwivedi, A. & Candler, G. V., 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3397. (2018 Fluid Dynamics Conference).

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

1 Scopus citations
2017

Global linear stability analysis of high speed flows on compression ramps

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

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

8 Scopus citations
2018

Slip effects in near continuum hypersonic flow over canonical geometries

Bhide, P. M., Singh, N., Nompelis, I., Schwartzentruber, T. & Candler, G., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

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

1 Scopus citations

Implementation of a nitrogen chemical kinetics model based on ab-initio data for hypersonic CFD

Chaudhry, R. S., Singh, N., Grover, M. S., Schwartzentruber, T. E. & Candler, G. V., 2018, 2018 Joint Thermophysics and Heat Transfer Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3439. (2018 Joint Thermophysics and Heat Transfer Conference).

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

7 Scopus citations
2017

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

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

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

4 Scopus citations
2018

Characterization of freestream disturbances in conventional hypersonic wind tunnels

Duan, L., Choudhari, M. M., Chou, A., Munoz, F., Ali, S. R. C., Radespiel, R., Schilden, T., Schröder, W., Marineau, E. C., Casper, K. M., Chaudhry, R. S., Candler, G. V., Gray, K. A., Sweeney, C. J. & Schneider, S. P., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

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

4 Scopus citations
2019

Receptivity analysis of bolt to distributed surface roughness using input-output analysis

Cook, D. A., Thome, J. S., Nichols, J. W. & Candler, G. V., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

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

Computations of measured pitot-probe spectra using angled freestream disturbances and comparisons to experiments

Chaudhry, R. S., Candler, G. V., Gray, K. A. & Schneider, S. P., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

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

2017

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, (47th AIAA Fluid Dynamics Conference, 2017).

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

2019

Input-output analysis of complex hypersonic boundary layers

Nichols, J. W. & Candler, G. V., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

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

2018

Sensitivity of hypersonic flows to distributed surface roughness using input-output analysis

Cook, D. A., Thome, J. S., Brock, J. M., Nichols, J. W. & Candler, G. V., Jan 1 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-4045. (2018 Fluid Dynamics Conference).

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

1 Scopus citations

Simulation and stability analysis of oblique shock-wave/boundary-layer interactions at Mach 5.92

Hildebrand, N., Dwivedi, A., Nichols, J. W., Jovanović, M. R. & Candler, G. V., Jan 2018, In : Physical Review Fluids. 3, 1, 013906.

Research output: Contribution to journalArticle

Open Access
8 Scopus citations
2019

Full Facility Shock Frame Simulations of the Electric Arc Shock Tube

Chandel, D., Brandis, A. & Candler, G. V., 2019.

Research output: Contribution to conferencePaper

2018

Wall-modeled large eddy simulation of supersonic combustion using flamelet/progress-variable modeling

Mrema, H. F. & Candler, G. V., 2018, 2018 Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-4561. (2018 Joint Propulsion Conference).

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

Input-output analysis of shock boundary layer interaction

Dwivedi, A., Sidharth, G. S., Candler, G. V., Nichols, J. W. & Jovanović, M. R., 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3220. (2018 Fluid Dynamics Conference).

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

2 Scopus citations
2017

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

Open Access
7 Scopus citations
2018

LES of the volvo combustion experiment with an ignition-delay variable

Candler, G. V., Kartha, A., Subbareddy, P. K. & Dimotakis, P. E., 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

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

3 Scopus citations
2019

Direct numerical simulation of high-speed transition due to roughness elements

Shrestha, P. & Candler, G. V., Jun 10 2019, In : Journal of Fluid Mechanics. 868, p. 762-788 27 p.

Research output: Contribution to journalArticle

2018

Subgrid-scale effects in compressible variable-density decaying turbulence

Sidharth, G. S. & Candler, G. V., Jul 10 2018, In : Journal of Fluid Mechanics. 846, p. 428-459 32 p.

Research output: Contribution to journalArticle

2 Scopus citations
2019

CFD Predictions of High Enthalpy Shocks in Nitrogen

Chandel, D., Nompelis, I., Candler, G. V. & Brandis, A., Jun 2019, AIAA Aviation 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2019-3078

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

2017

Assessment of predictive capabilities for aerodynamic heating in hypersonic flow

Knight, D., Chazot, O., Austin, J., Badr, M. A., Candler, G., 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 2017, In : Progress in Aerospace Sciences. 90, p. 39-53 15 p.

Research output: Contribution to journalReview article

29 Scopus citations
2019

Statistical analyses of quasiclassical trajectory data for air dissociation

Chaudhry, R. S. & Candler, G. V., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

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

1 Scopus citations
2018

Effects of freestream reynolds number and trip height on high-speed transition

Shrestha, P. & Candler, G. V., Jan 1 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3533. (2018 Fluid Dynamics Conference).

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

1 Scopus citations

Transient growth in oblique shock wave/laminar boundary layer interactions at mach 5.92

Hildebrand, N., Nichols, J. W., Candler, G. V. & Jovanović, M. R., Jan 1 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3221. (2018 Fluid Dynamics Conference).

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

1 Scopus citations
2017

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. (AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting).

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

2 Scopus 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

25 Scopus citations
2019

Estimation of inflow uncertainties in laminar hypersonic double-cone experiments

Ray, J., Kieweg, S., Dinzl, D., Carnes, B., Weirs, V. G., Freno, B., Howard, M., Smith, T., Nompelis, I. & Candler, G. V., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

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

1 Scopus citations

Large eddy simulation of supersonic combustion using the flamelet/progress-variable approach and the evolution-variable manifold approach

Mrema, H. F. & Candler, G. V., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

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

2018

Understanding effects of nose-cone bluntness on hypersonic boundary layer transition using input-output analysis

Cook, D. A., Thome, J. S., Brock, J. M., Nichols, J. W. & Candler, G. V., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

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

8 Scopus citations
2019

Boundary layer instabilities on bolt subscale geometry

Thome, J., Knutson, A. & Candler, G. V., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

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

1 Scopus citations

Freestream disturbance effects on boundary layer instability and transition on the afosr bolt geometry

Kostak, H. E., Bowersox, R. D. W., McKiernan, G. R., Thome, J., Candler, G. V. & King, R. A., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

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

2018

Direct numerical simulation of mach 6 flow over a cone with a highly swept fin

Knutson, A. L., Gs, S. & Candler, G. V., 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

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

6 Scopus citations
2017

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

Candler, G. V., Alba, C. R. & Greendyke, R. B., 2017, In : Journal of thermophysics and heat transfer. 31, 3, p. 512-526 15 p.

Research output: Contribution to journalArticle

6 Scopus citations