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

  • 5 Similar Profiles
Boundary layers Engineering & Materials Science
Direct numerical simulation Engineering & Materials Science
Reynolds number Engineering & Materials Science
Mach number Engineering & Materials Science
Flow control Engineering & Materials Science
Vortex flow Engineering & Materials Science
Airfoils Engineering & Materials Science
Turbulence Engineering & Materials Science

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Research Output 1973 2017

  • 2536 Citations
  • 25 h-Index
  • 171 Conference contribution
  • 60 Article
  • 10 Chapter

An efficient strategy for computing wave-packets in high-speed boundary layers

Browne, O. M. F., Haas, A. P., Fasel, H. F. & Brehm, C. 2017 47th AIAA Fluid Dynamics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: ResearchConference contribution

Wave packets
Boundary layer flow
Boundary layers
Hypersonic boundary layers
Geometry

A numerical jacobian stability solver based on the linearized compressible navier-stokes equations

Haas, A. P., Browne, O. M. F., Fasel, H. F. & Brehm, C. 2017 47th AIAA Fluid Dynamics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: ResearchConference contribution

Navier Stokes equations
Cones
Hypersonic boundary layers
Hypersonic flow
Angle of attack
1 Citations

Fundamental resonance breakdown for a flared cone at mach 6

Hader, C. & Fasel, H. F. 2017 AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., AIAA 2017-0765

Research output: ResearchConference contribution

Mach number
Cones
Direct numerical simulation
Tunnels
Experiments

Numerical investigation of the interaction of active flow control and klebanoff modes

Hosseinverdi, S. & Fasel, H. F. 2017 47th AIAA Fluid Dynamics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: ResearchConference contribution

Flow control
Turbulence
Direct numerical simulation
Transition flow
Laminar boundary layer

Numerical simulation of wing section undergoing plunging motions at high angles of attack

Gross, A., Little, J. & Fasel, H. 2017 47th AIAA Fluid Dynamics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: ResearchConference contribution

Angle of attack
Computer simulation
Vortex flow
Flow separation
Aerodynamic loads