Hermann F. Fasel

Professor of Aerospace and Mechanical Engineering
Degrees
 Ph.D.
Courses
Dissertation
AME 920 (Spring 2018)
AME 920 (Fall 2017)
AME 920 (Spring 2017)
AME 920 (Fall 2016)
Independent Study
AME 599 (Spring 2018)
AME 799 (Spring 2018)
AME 599 (Fall 2017)
AME 699 (Spring 2017)
AME 599 (Spring 2017)
AME 499 (Fall 2016)
AME 399 (Fall 2016)
AME 699 (Fall 2016)
AME 599 (Fall 2016)
Research
AME 900 (Spring 2018)
AME 900 (Fall 2017)
AME 900 (Spring 2017)
AME 900 (Fall 2016)
Thesis
AME 910 (Spring 2018)
AME 910 (Fall 2017)
AME 910 (Fall 2016)
AME 910 (Summer I 2016)
Directed Research
AME 492 (Summer I 2017)
AME 492 (Spring 2017)
Aircraft Performance
AME 321 (Spring 2017)
Num Mth Fld Mech+Ht Trsf
AME 431 (Spring 2017)
AME 531 (Spring 2017)
Selected Publications
Journals/Publications
 Fasel, H. F., & Balzer, W. (2016). Numerical Investigation of the Role of Freestream Turbulence in Boundarylayer Separation. Journal of Fluid Mechanics, 801, Page no. 289321.
 Fasel, H. F., & Gross, A. (2016). Hybrid Turbulence Model Simulations of Partially Stalled Airfoil Flow. AIAA Journal, 54(4), Page no. 12201234.
 Fasel, H. F., & Gross, A. (2016). Numerical Investigation of Shock BoundaryLayer Interactions. AIAA 20160347.
 Fasel, H. F., & Hader, C. (2016). LaminarTurbulent Transition on a Flared Cone at Mach 6. AIAA 20163344.
 Fasel, H. F., & Hoseinverdi, S. (2016). Direct Numerical Simulations of LaminartoTurbulent Transition in Laminar Separation Bubbles in ThreeDimensional BoundaryLayer. AIAA20163793.
 Fasel, H. F., & Laible, A. (2016). Continuously Forced Transient Growth in Oblique Breakdown for Supersonic Boundary Layers. Journal of Fluid Mechanics, 804, Page no. 323350.
 Fasel, H. F., & Sivasubramanian, J. (2016). Direct Numerical Simulation of LaminarTurbulent Transition in a Flared Cone Boundary Layer at Mach 6. AIAA 20160846.
 Fasel, H. F., & Sivasubramanian, J. (2016). Numerical Investigation of Shockwave Boundary Layer Interactions in Supersonic Flows. AIAA 20160613.
 Fasel, H. F., Gross, A., & Little, J. (2016). Numerical Simulation of Wing Section Near Stall. AIAA 20163947.
 Fasel, H. F., Mertens, C., Pineda, S., Little, J. C., & Gross, A. (2016). Effects of Structural Motion on the Aerodynamics of the X56A Airfoil. AIAA 20162073.
 Tumin, A., Fasel, H. F., & Sivasubramanian, J. (2016). The Reynolds Number Effect on Receptivity to a Localized Disturbance in a Hypersonic Boundary Layer. AIAA Paper No. 20164246.
 Embacher, M., & Fasel, H. F. (2014). Direct Numerical Simulations of Laminar Separation Bubbles: Investigation of Absolute Instability and Active Flow Control of Transition to Turbulence. Journal of Fluid Mechanics, 747, 141185.
 Mayer, C. J., Fasel, H. F., Choudhari, M., & Chang, C. L. (2014). Transition Onset Predictions for Oblique Breakdown in a Mach 3 Boundary Layer. AIAA Journal, 52(4), 882885.
 Sivasubramanian, J., & Fasel, H. F. (2014). Numerical Investigation of the Development of Threedimensional Wavepackets in a Sharp Cone Boundary Layer at Mach 6. Journal of Fluid Mechanics, 756, 600649.
 Balzer, W., & Fasel, H. F. (2013). Direct numerical simulations of laminar separation bubbles on a curved plate: Part 1  Simulation setup and uncontrolled flow. Proceedings of the ASME Turbo Expo, 6 B.
Proceedings Publications
 Balthazar, M., Gross, A., & Fasel, H. F. (2014, January 1317). Experimental Investigation of Flows with Threedimensional Separation. In 52nd AIAA Aerospace Sciences Meeting.
 Brehm, C., Hader, C., & Fasel, H. F. (2014, January 1317). A Highorder Immersed Interface Method for Compressible Flows. In 52nd Aerospace Sciences Meeting.
 Fasel, H. F., Sivasubramanian, J., & Laible, A. (2014, September 812). Numerical Investigation of Transition in a Flared Cone Boundary Layer at Mach 6. In IUTAMABCM Symposium on LaminarTurbulent Transition.
 Gross, A., & Fasel, H. F. (2014, January 1317). Hybrid Turbulence Model Simulations of Internal and External Flows. In 52nd AIAA Aerospace Sciences Meeting.
 Hader, C., Brehm, C., & Fasel, H. F. (2014, June 1620). Numerical Investigation of Transition Delay for Various Controlled Breakdown Scenarios in a Mach 6 Boundary Layer Using Porous Walls. In 7th AIAA Theoretical Fluid Mechanics Conference.
 Hass, A. P., Gross, A., & Fasel, H. F. (2014, June 1620). Numerical Investigation of the Threedimensional Vertical Flow for an Ellipsoid Model. In 32nd AIAA Applied Aerodynamics Conference.
 Salami, L., Fasel, H. F., Wernz, S., & Marquart, E. (2014, June 1620). Numerical Investigations of Wavepackets in a Hypersonic HIghenthalpy Boundary Layer on a 5 deg Sharp Cone. In 7th AIAA Theoretical Fluid Mechanics Conference.
 Salemi, L., Gross, A., Fasel, H. F., Wernz, S., & Marquart, E. (2014, January 1317). Linearized NavierStokes Calculations of the Spatial Stability of a Hypersonic Boundary Layer on a 5^o Sharp Cone with High Temperature Effects. In 52nd Aerospace Sciences Meeting.
 Shirzad, H., & Fasel, H. F. (2014, September 812). Laminarturbulent Transition in a Laminar Separation Bubble in the Presence of Freestream Turbulence. In IUTAMABCM Symposium on LaminarTurbulent Transition.
Presentations
 Fasel, H. F. (2016, April). Direct Numerical Simulations of Nonlinear transition for a flared cone. AVTNATO workshop on Second Mode hypersonic Transition. South Bend, IN: Notre Dame.
 Fasel, H. F. (2016, August). DNS of stability and transition for hypersonic boundary layers. AFOSR Conference on high speed flows and turbulence. Washington, DC.
 Fasel, H. F. (2016, July). Effect of structural motion on the flow physics of transition an separation. AFOSR Conference on Flow Physics and Control. Arlington, VA.
 Fasel, H. F. (2016, October). Investigation of transition in highspeed and high enthalpy flows. CTS Workshop on Experimental and Numerical investifation of Boundary Layer Transition. Tullahoma, TN.
 Fasel, H. F. (2016, October). Stability and transition investigations of HighEnthalpy flows. AVTNATO  240 Congress. Avila, Spain.
 Fasel, H. F., Little, J. C., & Gross, A. (2016, June). Impact of Structural Motion on Separation and Separation Control: Integrated Investigation using Numerical Simulations, Theory, Windtunnel and Freeflight Experiments. AFOSR/ARO Review Meeting. Arlington, VA: AFOSR/ARO.
 Little, J. C., Fasel, H. F., & Gross, A. (2016, June). Investigation of 3D ShockBoundary Layer Interaction: A Combined Approach using Experiments, Numerical Simulations and Stability Analysis. AFOSR/ONR Review Meeting. Arlington, VA: AFOSR/ONR.
 Fasel, H. F. (2014, July 2931). Investigation of Boundarylayer Separation: Its Control. AFOSR Flow Interactions and Control Workshop. Arlington, VA: AFOSR.
 Fasel, H. F. (2014, June 19). Investigation of Highspeed Boundarylayer Stability and Transition Using Direct Numerical Simulations. Seminar. Stuttgart, Germany.
 Fasel, H. F. (2014, March 1921). Direct Numerical Simulation of Laminarturbulent Transition for a Cone at M6. Symposium on Nonlinear Stability Theory: From Weakly Nonlinear Theory to the Verge of Turbulence. London, UK: Imperial College.