• 2933 Citations
  • 26 h-Index
1973 …2018
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  • 3 Similar Profiles
Direct numerical simulation Engineering & Materials Science
Boundary layers Engineering & Materials Science
Mach number Engineering & Materials Science
Reynolds number Engineering & Materials Science
Flow control Engineering & Materials Science
Airfoils Engineering & Materials Science
Navier Stokes equations Engineering & Materials Science
Vortex flow Engineering & Materials Science

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Research Output 1973 2018

  • 2933 Citations
  • 26 h-Index
  • 175 Conference contribution
  • 65 Article
  • 7 Chapter
1 Citations

Active flow control of the laminar separation bubble on an oscillating airfoil near stall

Agate, M. A., Pande, A., Little, J. C., Fasel, H. F. & Gross, A., 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

Airfoils
Flow control
Blow molding
Experiments
Computer simulation

A history and progress of research on boundary-layer transition on a mach 6 flared cone

Chynoweth, B. C., Schneider, S. P., Hader, C., Fasel, H., Batista, A., Kuehl, J., Juliano, T. J. & Wheaton, B. 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

Mach number
Cones
Boundary layers
Heating
Wave packets
multigrid methods
Poisson equation
Computational efficiency
mesh
grids

Hypersonic boundary-layer transition: Comparison of the fundamental resonance breakdown for a flared and straight cone at mach 6

Meersman, J. A., Hader, C. & Fasel, H. F., Jan 1 2018, 2018 Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3851

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

Hypersonic boundary layers
Mach number
Cones
Tunnels
Geometry
1 Citations

Numerical investigation of shock wave turbulent boundary layer interactions

Gross, A., Little, J. C. & Fasel, H. F., 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 waves
Boundary layers
Reynolds number
Supersonic flow
Large eddy simulation