• 2832 Citations
  • 26 h-Index
1973 …2018
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Fingerprint Fingerprint is based on mining the text of the experts' scientific documents to create an index of weighted terms, which defines the key subjects of each individual researcher.

  • 2 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

  • 2832 Citations
  • 26 h-Index
  • 174 Conference contribution
  • 62 Article
  • 7 Chapter

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

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

Numerical simulation of plunging wing section at high angles of attack

Gross, A., Agate, M., Little, J. & Fasel, H. F. Jan 1 2018 In : AIAA journal. 56, 7, p. 2514-2527 14 p.

Research output: Contribution to journalArticle

Angle of attack
Computer simulation
Vortex flow
Aerodynamic loads
Flow separation
Hypersonic boundary layers
hypersonic boundary layer
Direct numerical simulation
disturbances
breakdown