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Author

  • Graham V Candler
2018

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
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
2016

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

Shrestha, P. & Candler, G., 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

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

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

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

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
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
2017

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
2018

Onset of three-dimensionality in supersonic flow over a slender double wedge

Gs, S., Dwivedi, A., Candler, G. V. & Nichols, J. W., Sep 2018, In : Physical Review Fluids. 3, 9, 093802.

Research output: Contribution to journalArticle

Open Access
4 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
2019

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
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

Instabilities in mach 6 flow over a cone with a swept fin

Knutson, A. L., Sidharth, G. S. & Candler, G. V., 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3071. (2018 Fluid Dynamics Conference).

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

3 Scopus citations
2019

Nonequilibrium flow through porous thermal protection materials, Part II: Oxidation and pyrolysis

Poovathingal, S., Stern, E. C., Nompelis, I., Schwartzentruber, T. E. & Candler, G. V., Mar 1 2019, In : Journal of Computational Physics. 380, p. 427-441 15 p.

Research output: Contribution to journalArticle

2 Scopus citations
2018

Quasiclassical trajectory analysis of oxygen dissociation via O2,O, and N2

Chaudhry, R. S., Grover, M. S., Bender, J. D., Schwartzentruber, T. E. & 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

17 Scopus citations
2017

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
2020

Transient growth analysis of oblique shock-wave/boundary-layer interactions at Mach 5.92

Dwivedi, A., Hildebrand, N., Nichols, J. W., Candler, G. V. & Jovanović, M. R., Jun 2020, In : Physical Review Fluids. 5, 6, 063904.

Research output: Contribution to journalArticle

Numerical simulations of shock propagation under strong nonequilibrium conditions

Chandel, D., Nompelis, I. & Candler, G. V., 2020, In : Journal of thermophysics and heat transfer. 34, 3, p. 556-569 14 p.

Research output: Contribution to journalArticle

2019

Reattachment streaks in hypersonic compression ramp flow: An input-output analysis

Dwivedi, A., Sidharth, G. S., Nichols, J. W., Candler, G. V. & Jovanović, M. R., Jan 1 2019, (Accepted/In press) In : Journal of Fluid Mechanics. p. 113-135 23 p.

Research output: Contribution to journalArticle

5 Scopus citations