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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.

  • 6 Similar Profiles
Hypersonic aerodynamics Engineering & Materials Science
Mach number Engineering & Materials Science
Hypersonic flow Engineering & Materials Science
Boundary layers Engineering & Materials Science
Computational fluid dynamics Engineering & Materials Science
Cones Engineering & Materials Science
Reynolds number Engineering & Materials Science
Experiments Engineering & Materials Science

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Projects 2004 2022

Research Output 1988 2018

An improved ducros sensor for the simulation of compressible flows with shocks

Hendrickson, T. A., Kartha, A. & Candler, G. V., Jan 1 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3710

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

Compressible flow
Sensors
Vorticity
Turbulent flow
Switches
1 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

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

Hypersonic aerodynamics
Wind tunnels
Mach number
Enthalpy
Boundary layers

Computational study of high speed flow on a sliced cone-flap geometry

Thome, J., Reinert, J. D., Dwivedi, A. & Candler, G. V., Jan 1 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3397

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

Hypersonic vehicles
Flaps
Control surfaces
Surface measurement
Hypersonic aerodynamics

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

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

Shock tubes
Electric arcs
NASA
Enthalpy
Pipe flow
1 Citations

Direct numerical simulation of BOLT hypersonic flight vehicle

Thome, J., Dwivedi, A., Nichols, J. W. & Candler, G. V., Jan 1 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-2894

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

Hypersonic aerodynamics
Direct numerical simulation
Boundary layers
Laminar boundary layer
Reynolds number