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Author

  • Graham V Candler
2015

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. (53rd AIAA Aerospace Sciences Meeting).

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

15 Scopus citations
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

2011

Numerical simulations of transition experiments in the hypersonic ballistic range

Yoon, S., Barnhardt, M. D., Sozer, E. & Candler, G. V., Dec 1 2011, 41st AIAA Fluid Dynamics Conference and Exhibit. (41st AIAA Fluid Dynamics Conference and Exhibit).

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

1 Scopus citations
2014

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., (44th AIAA Fluid Dynamics Conference).

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

4 Scopus citations
2011

Hybrid reynolds-averaged and large-eddy simulation of scramjet fuel injection

Peterson, D. M., Tylczak, E. B. & Candler, G. V., Dec 1 2011, 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011. (17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011).

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

14 Scopus citations
2018

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
2011

Hypersonic three-dimensional boundary layer transition on a cone at angle of attack

Gronvall, J. E., Johnson, H. B. & Candler, G. V., Dec 1 2011, 41st AIAA Fluid Dynamics Conference and Exhibit. (41st AIAA Fluid Dynamics Conference and Exhibit).

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

6 Scopus citations

DNS of transition to turbulence in a hypersonic boundary layer

Subbareddy, P. K. & Candler, G. V., Dec 1 2011, 41st AIAA Fluid Dynamics Conference and Exhibit. (41st AIAA Fluid Dynamics Conference and Exhibit).

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

1 Scopus citations
2014

Microscale simulations of porous TPS materials: Application to permeability

Stern, E. C., Nompelis, I., Schwartzentruber, T. E. & Candler, G. V., 2014, AIAA AVIATION 2014 -11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference. American Institute of Aeronautics and Astronautics Inc., (AIAA AVIATION 2014 -11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference).

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

5 Scopus citations
2012
21 Scopus citations
2019

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

2014

Quasiclassical trajectory analysis of the N2 + N2 reaction using a new ab initio potential energy surface

Bender, J. D., Nompelis, I., Valentini, P., Schwartzentruber, T., Candler, G. V., Doraiswamy, S., Paukku, Y., Yang, K. R., Varga, Z. & Truhlar, D. G., Jan 1 2014, AIAA AVIATION 2014 -11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference. American Institute of Aeronautics and Astronautics Inc., (AIAA AVIATION 2014 -11th AIAA/ASME Joint Thermophysics and Heat Transfer Conference).

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

12 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
2013

Numerical simulation of drogue parachute in the wake of the multi-purpose crew vehicle

Dinzl, D. J., Gidzak, V. M. & Candler, G. V., Aug 2 2013, AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013. (AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013).

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

2016

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, (54th AIAA Aerospace Sciences Meeting).

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

5 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

2015

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. (53rd AIAA Aerospace Sciences Meeting).

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

50 Scopus citations
2013

Wake-fabric interactions in ADEPT-VITaL

Gidzak, V. M. & Candler, G. V., Aug 2 2013, AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013. (AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013).

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

1 Scopus citations
2014

Subgrid-scale modeling of baroclinic vorticity

Sidharth, G. S., Candler, G. V. & Dimotakis, P. E., Jan 1 2014, AIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference. American Institute of Aeronautics and Astronautics Inc., (AIAA AVIATION 2014 -7th AIAA Theoretical Fluid Mechanics Conference).

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

2011

Roughness-induced instabilities at Mach 6: A combined numerical and experimental study

Wheaton, B. M., Bartkowicz, M. D., Subbareddy, P. K., Schneider, S. P. & Candler, G. V., Dec 1 2011, 41st AIAA Fluid Dynamics Conference and Exhibit. (41st AIAA Fluid Dynamics Conference and Exhibit).

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

24 Scopus citations

Direct numerical simulation of transient growth on a flat plate at Mach 3

Wagnild, R. & Candler, G. V., Dec 1 2011, 41st AIAA Fluid Dynamics Conference and Exhibit. (41st AIAA Fluid Dynamics Conference and Exhibit).

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

2016

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

2 Scopus citations
2015

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

4 Scopus citations
2017

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
2011

Numerical simulation of hypersonic capsule base flow

Brock, J. M., Subbareddy, P. K. & Candler, G. V., Dec 1 2011, 42nd AIAA Thermophysics Conference. (42nd AIAA Thermophysics Conference).

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
2015

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

8 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
2015

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

16 Scopus citations
2017

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
2013

Decoupled implicit method for aerothermodynamics and reacting flows

Candler, G. V., Subbareddy, P. K. & Nompelis, I., May 1 2013, In : AIAA journal. 51, 5, p. 1245-1254 10 p.

Research output: Contribution to journalArticle

22 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

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

2015

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

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

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

3 Scopus citations
2012

Development of a Mach 5 nonequilibrium-flow wind tunnel

Nishihara, M., Takashima, K., Jiang, N., Lempert, W. R., Adamovich, I. V., Rich, J. W., Doraiswamy, S. & Candler, G. V., Oct 2012, In : AIAA journal. 50, 10, p. 2255-2267 13 p.

Research output: Contribution to journalArticle

16 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

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
2014

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

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

Research output: Contribution to journalArticle

9 Scopus citations
2012

Detached-eddy simulation of the reentry-F flight experiment

Barnhardt, M. & Candler, G. V., 2012, In : Journal of Spacecraft and Rockets. 49, 4, p. 691-699 9 p.

Research output: Contribution to journalArticle

11 Scopus citations
2013

LES of a high-Reynolds number, chemically reacting mixing layer

Ferrero, P., Kartha, A., Subbareddy, P. K., Candler, G. V. & Dimotakis, P. E., Sep 11 2013, 43rd Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc., (43rd 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

2019

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
2011

Numerical simulation of hypersonic shock wave-boundary-layer interactions

Candler, G. V., Jan 1 2011, Shock Wave-Boundary-Layer Interactions. Cambridge University Press, p. 314-335 22 p.

Research output: Chapter in Book/Report/Conference proceedingChapter

3 Scopus citations
2018

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
2016

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

Komives, J. R., Subbareddy, P. K. & Candler, G. V., 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (54th AIAA Aerospace Sciences Meeting; vol. 0).

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

2 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
2018

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