Fingerprint The Fingerprint is created by mining the titles and abstracts of the person's research outputs and projects/funding awards to create an index of weighted terms from discipline-specific thesauri.

  • 6 Similar Profiles
Experiments Engineering & Materials Science
Hypersonic aerodynamics Engineering & Materials Science
Boundary layers Engineering & Materials Science
Mach number Engineering & Materials Science
Computational fluid dynamics Engineering & Materials Science
simulation Physics & Astronomy
Cones Engineering & Materials Science
Temperature Engineering & Materials Science

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Projects 2004 2020

hypersonic flow
boundary layer
surface reactions
Hypersonic aerodynamics
Laminar flow
Flow control

Research Output 1988 2017

2 Citations

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. Feb 3 2017 (Accepted/In press) In : Progress in Aerospace Sciences.

Research output: Research - peer-reviewArticle

Aerodynamic heating
Hypersonic flow
Hypersonic aerodynamics
Computational fluid dynamics
Plant startup

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: Research - peer-reviewArticle

reaction kinetics
vapor phases

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: Research - peer-reviewArticle

Parallel flow
Hypersonic aerodynamics
Transfer functions
Natural frequencies
Numerical methods

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: ResearchConference contribution

Mach number
Heat transfer
Hypersonic inlets
Hypersonic vehicles

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: Research - peer-reviewArticle

Hypersonic aerodynamics
Surface roughness
Reynolds number