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  • Graham V Candler

A decoupled implicit method for aerothermodynamics and reacting flows

Candler, G. V., Subbareddy, P. K. & Nompelis, I., Dec 1 2012, 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012.

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

1 Scopus citations

A decoupled implicit method for aerothermodynamics and reacting flows

Candler, G. V., Subbareddy, P. K. & Nompelis, I., 2012, 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. American Institute of Aeronautics and Astronautics Inc., (18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012).

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

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

27 Scopus citations

A generalized chemistry - internal energy coupling model using prior recombination distribution

Doraiswamy, S., Kelley, J. D. & Candler, G. V., Jan 1 2012, 43rd AIAA Thermophysics Conference 2012. American Institute of Aeronautics and Astronautics Inc., (43rd AIAA Thermophysics Conference 2012).

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

Analysis of a decoupled implicit method for aerothermodynamics and reacting flows

Candler, G. V., Subbareddy, P. K. & Nompelis, I., Aug 19 2013, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013. American Institute of Aeronautics and Astronautics Inc., (51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013).

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

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

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., 2016, 46th AIAA Thermophysics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, (46th AIAA Thermophysics Conference).

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

4 Scopus citations

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
85 Scopus citations

An investigation into a non-axisymmetric tension shell decelerator concept via a computational design procedure

Gidzak, V. M. & Candler, G. V., Dec 1 2011, 29th AIAA Applied Aerodynamics Conference 2011. American Institute of Aeronautics and Astronautics Inc., (29th AIAA Applied Aerodynamics Conference 2011).

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

A novel simulation approach for the AEDC hypervelocity tunnel 9 Mach 14 nozzle

Boe, K. & Candler, G. V., Jan 1 2011, 41st AIAA Fluid Dynamics Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc., (41st AIAA Fluid Dynamics Conference and Exhibit).

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

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, (46th AIAA Fluid Dynamics Conference).

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

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

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

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

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, (20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015).

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

CFD-based axisymmetric aeroshell shape optimization in hypersonic entry conditions

Neville, A. G. & Candler, G. V., 2013, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013. American Institute of Aeronautics and Astronautics Inc., (51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013).

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

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

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

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

Characterization of freestream disturbances in conventional hypersonic wind tunnels

Duan, L., Choudhari, M. M., Chou, A., Munoz, F., Radespiel, R., Schilden, T., Schröder, W., Marineau, E. C., Casper, K. M., Chaudhry, R. S., Candler, G. V., Gray, K. A. & Schneider, S. P., 2019, In : Journal of Spacecraft and Rockets. 56, 2, p. 357-368 12 p.

Research output: Contribution to journalArticle

Open Access
5 Scopus citations

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

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

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

4 Scopus 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

8 Scopus citations

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., (52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014).

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

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

2 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

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

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

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

Research output: Contribution to journalArticle

8 Scopus citations

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

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

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

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

Research output: Contribution to journalArticle

5 Scopus citations

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

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

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

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

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

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., 086102.

Research output: Contribution to journalArticle

59 Scopus citations

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

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

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

Subbareddy, P. K., Bartkowicz, M. D. & Candler, G. V., Apr 28 2014, In : Journal of Fluid Mechanics. 748, 3, p. 848-878 31 p.

Research output: Contribution to journalArticle

41 Scopus citations

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

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

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

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

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

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. (53rd AIAA Aerospace Sciences Meeting).

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

DNS of transition to turbulence in a Mach 6 Boundary layer

Subbareddy, P. K. & Candler, G. V., 2012, 43rd AIAA Thermophysics Conference 2012. American Institute of Aeronautics and Astronautics Inc., (43rd AIAA Thermophysics Conference 2012).

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

3 Scopus citations