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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.

  • 9 Similar Profiles
Hypersonic aerodynamics Engineering & Materials Science
Boundary layers Engineering & Materials Science
Mach number Engineering & Materials Science
Hypersonic flow Engineering & Materials Science
Computational fluid dynamics Engineering & Materials Science
Cones Engineering & Materials Science
Experiments Engineering & Materials Science
Direct numerical simulation Engineering & Materials Science

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Projects 2004 2022

Research Output 1988 2019

Boundary layer instabilities on bolt subscale geometry

Thome, J., Knutson, A. L. & 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

Bolts
Mach number
Boundary layers
Decomposition
Geometry
2 Citations (Scopus)

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., Jan 1 2019, In : Journal of Spacecraft and Rockets. 56, 2, p. 357-368 12 p.

Research output: Contribution to journalArticle

Open Access
hypersonic wind tunnels
Hypersonic aerodynamics
wind tunnel
boundary layer transition
Mach number

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

Acoustics
Hypersonic flow
Geometry
Direct numerical simulation
Wind tunnels

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

Diamond
Direct numerical simulation
direct numerical simulation
Vortex flow
roughness

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

Hypersonic aerodynamics
Cones
Wind tunnels
Experiments
Fluid dynamics