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Fingerprint Fingerprint is based on mining the text of the expert's scholarly documents to create an index of weighted terms, which defines the key subjects of each individual researcher.

  • 3 Similar Profiles
Velocity measurement Engineering & Materials Science
Mach number Engineering & Materials Science
Boundary layers Engineering & Materials Science
Turbulence Engineering & Materials Science
shear layers Physics & Astronomy
base flow Physics & Astronomy
Supersonic flow Engineering & Materials Science
Vortex flow Engineering & Materials Science

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Research Output 1975 2019

Three-component turbulence measurements and analysis of a supersonic, axisymmetric base flow

Kirchner, B. M., Favale, J. V., Elliott, G. S. & Dutton, J. C., Jan 1 2019, In : AIAA journal. 57, 6, p. 2496-2512 17 p.

Research output: Contribution to journalArticle

Velocity measurement
Flow fields
Turbulence
Statistics
Uncertainty analysis

A three-dimensional experimental study of compressibility effects on turbulent free shear layers

Kim, K. U., Elliott, G. S. & Dutton, J. C., Jan 1 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3864

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

Compressibility
Anisotropy
Flow visualization
Velocity measurement
Mach number

Flow structure identification in the near wake of a supersonic separated flow using FAEMD

Koll, M. D., Scott, A. P., Elliott, G. S. & Dutton, J. C., Jan 1 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3540

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

Supersonic flow
Flow structure
Vortex flow
Decomposition
Velocity measurement

Simultaneous flowfield and surface-deflection measurementsofan axisymmetric jet and adjacent surface

Hortensius, R., Dutton, J. C. & Elliott, G. S., Jan 1 2018, In : AIAA journal. 56, 3, p. 917-932 16 p.

Research output: Contribution to journalArticle

Boundary layers
Fluid structure interaction
Surface measurement
Pressure measurement
Velocity measurement

Three-dimensional structure of the compressible mixing layer of an axisymmetric, supersonic, separated flow

Kirchner, B. M., Tetef, T. J., Elliott, G. S. & Dutton, J. C., Jan 1 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3084

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

Supersonic flow
Flow fields
Velocity measurement
Pressure gradient
Flow control