Hermann F. Fasel

Journals/Publications

• Fasel, H. F. (2021). 10) Haas, A. P., Hader, C., Fasel, H. F. “Linear Stability Investigation of Cross-Flow Instability for a Supersonic Swept Wing with a Biconvex Airfoil,” AIAA 2021-2848, 2021. AIAA.
• Fasel, H. F. (2021). 11) Hader, C., Fasel, H. F. “Flow control using steady blowing and suction strips in a Mach 6 Boundary Layer on a Flared Cone.” AIAA 2021-1206, 2021. AIAA.
• Fasel, H. F. (2021). 12) Hader, C., Deng, N., Fasel, H. F. “Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a straight cone at Mach 5.” AIAA 2021-0743, 2021. AIAA.
• Fasel, H. F. (2021). 13) Hader, C., Deng, N., Woodward, M., Fasel, H. F. “Direct Numerical Simulations of Laminar-Turbulent Transition for Transonic Boundary Layers,” AIAA 2021- 1658, 2021. AIAA.
• Fasel, H. F. (2021). 14) Hartman, A., Hader, C., Fasel, H. F. “Direct Numerical Simulations of laminar-turbulent boundary-layer transition for a blunt cone at Mach 6,” AIAA 2021-0744, 2021. AIAA.
• Fasel, H. F. (2021). 15) Leinemann, M., Hader, C., Fasel, H. F. “Direct Numerical Simulations of the Nonlinear Boundary Layer Transition Regime on a Flat Plate at Mach 6,” AIAA 2021- 1739, 2021. AIAA.
• Fasel, H. F. (2021). 16) Hosseinverdi, S. & Fasel, H. F. “High-Order accurate incompressible Navier-Stokes solver based on vorticity-velocity formulation for orthogonal curvilinear grids,” AIAA 2021-2741, 2021. AIAA.
• Fasel, H. F. (2021). 17) Bahrainirad, L., Hosseinverdi, S., & Fasel, H. F. “Wave Packet Development in Three-Dimensional Low-Speed Laminar Boundary Layers,” AIAA 2021-2897, 2021. AIAA.
• Fasel, H. F. (2021). 18) Borgmann, D., Hosseinverdi, S., Little, J. C. & Fasel, H. F. “Investigation of laminar separation bubbles using experiments, theory and DNS,” AIAA 2021-2898, 2021. AIAA.
• Fasel, H. F. (2021). 19) Guerra, A. G., Hosseinverdi, S., Singh, A., Little, J. C. & Fasel, H. F. “Unsteady evolution of a laminar separation bubble subjected to structural motion,” AIAA 2021-2949, 2021. AIAA.
• Fasel, H. F. (2021). 2) Meersman, J.A., Hader, C., Fasel, H.F. “Numerical investigation of Nonlinear Boundary-Layer Transition for Cones at Mach 6,” AIAA Journal Vol. 59 No. 6: 1940-1952, 2021.. AIAA J., 59, 1940-1952.
• Fasel, H. F. (2021). 3) Gross, A., and Fasel, H.F., “Numerical Investigation of Wing Section Undergoing Low-Frequency Aeroelastic Limit Cycle Oscillations,” AIAA Journal, Vol. 59, No. 4, pp. 1361-1373, 2021. AIAA J., 59.
• Fasel, H. F. (2021). 4) Meersman, J. A., Hader, C., & Fasel, H. F. “Direct Numerical Simulations of Nonlinear Entropy-Layer Instability Waves,” AIAA 2021-1737, 2021. AIAA.
• Fasel, H. F. (2021). 5) Hader, C., Fasel, H. F. “Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Straight Cone at Mach 4: Oblique Breakdown,” AIAA 2021-2863, 2021. AIAA.
• Fasel, H. F. (2021). 6) Hader, C., Fasel, H. F. “Direct Numerical Simulations of Hypersonic Boundary-Layer Transition for a Straight Cone at Mach 7,” AIAA 2021-2865, 2021. AIAA.

Proceedings Publications

• Fasel, H. F., Tumin, A., & Sivasubramanian, J. (2016, June). The Reynolds Number Effect on Receptivity to a Localized Disturbance in a Hypersonic Boundary Layer. In AIAA Paper No. 2016-4246.
• Balthazar, M., Gross, A., & Fasel, H. F. (2014, January 13-17). Experimental Investigation of Flows with Three-dimensional Separation. In 52nd AIAA Aerospace Sciences Meeting.
• Brehm, C., Hader, C., & Fasel, H. F. (2014, January 13-17). A High-order Immersed Interface Method for Compressible Flows. In 52nd Aerospace Sciences Meeting.
• Fasel, H. F., Sivasubramanian, J., & Laible, A. (2014, September 8-12). Numerical Investigation of Transition in a Flared Cone Boundary Layer at Mach 6. In IUTAM-ABCM Symposium on Laminar-Turbulent Transition.
• Gross, A., & Fasel, H. F. (2014, January 13-17). Hybrid Turbulence Model Simulations of Internal and External Flows. In 52nd AIAA Aerospace Sciences Meeting.
• Hader, C., Brehm, C., & Fasel, H. F. (2014, June 16-20). 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 16-20). Numerical Investigation of the Three-dimensional Vertical Flow for an Ellipsoid Model. In 32nd AIAA Applied Aerodynamics Conference.
• Salami, L., Fasel, H. F., Wernz, S., & Marquart, E. (2014, June 16-20). Numerical Investigations of Wavepackets in a Hypersonic HIgh-enthalpy 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 13-17). Linearized Navier-Stokes 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 8-12). Laminar-turbulent Transition in a Laminar Separation Bubble in the Presence of Free-stream Turbulence. In IUTAM-ABCM Symposium on Laminar-Turbulent Transition.

Presentations

• Bailey, M. (2019, September). Numerical investigation of the nonlinear transition stages in a high enthalpy boundary layer,. IUTAM Symposium on Laminar-Turbulent Transition. London, UK: IUTAM.
• Fasel, H. F. (2019, July). Investigation of Laminar-Turbulent Transition for Transonic Boundary Layers Using Advanced Computational Tools. ARO Fluid Dynamics Program Review. Colorado Springs: Army Research Office.
• Fasel, H. F. (2019, July). Numerical Investigations of the Nonlinear Transition Stages in Hypersonic Boundary Layers for Navy Relevant Mach Numbers and Model Geometrics. ONR Program Review for High-Speed Flows. Boulder, CO: Office of Naval Research.
• Fasel, H. F. (2019, June). Direct numerical simulations for understanding complex flow phenomena. AIAA Aviation Conference. Dallas, TX: AIAA.
• Fasel, H. F. (2019, September). Investigation of laminar-turbulent transition using high-fidelity direct numerical simulations. German Symposium on Hypersonic Transition. Munich, Germany.
• Hader, C. (2019, July). Numerical Investigation of Nonlinear Transition Stages in Hypersonic Boundary Layers for Wind-Tunnel and Free-Flight Conditions. AFOSR Workshop on High-Speed Flows and Turbulence. Boulder, CO: Airforce office of Scientific Research.
• Hader, C. (2019, September). DNS of natural transition in high-speed boundary layers. IUTAM Symposium on Laminar Turbulent Transition. London, UK: IUTAM.
• Hosseinverdi, S. (2019, September). Towards understanding of natural boundary-layer transition via random excitation. IUTAM Symposium on Laminar-Turbulent Transition. London, UK: IUTAM.
• Little, J. (2019, July). Wing Sweep, Structural Motion and Their Effect on Separation and Transition - Simulations, Wind Tunnel and Flight Experiments. AFOSR Program Review for low speed flows and Flow Control. Colorado Springs: Air Force Ofiice of Scientific Research.
• Agate, M., Pande, A., Little, J., & Gross, A. (2018, June). Agate, M., Pande, A., Little, J.C., Gross, A., and Fasel, H.F., “Active flow control of the laminar separation bubble on an oscillating airfoil near stall. 56th AIAA Aerospace Sciences Meeting, AIAA-2018-2049, 2018. 56th AIAA Aerospace Sciences Meeting. Atlanta: AIAA.
• Fasel, H. F. (2018, January). Role of Klebanoff modes in active control of laminar separation bubbles.. 13th ERCOFTAC SIG 33 Workshop, Progress in Flow Instability, Transition and Control. Paraty, Brazil: ERCOFTAC.
• Fasel, H. F. (2018, July). Numerical Investigation of Nonlinear Boundary Layer transition. AFOSR/ONR High-Speed Research Review. Washingtion DC: AFOSR/ONR.
• Fasel, H. F. (2018, june). Numerical investigation of boundary-layer transition and separation using controlled disturbance input. Invited talk. 48th AIAA Fluid Dynamics Conference. Atlanta: AIAA.
• Gross, A., & Little, J. (2018, january). 1. Gross, A., Little, J. & Fasel, H. F. Numerical investigation of shock wave turbulent boundary layer interactions. 2018 AIAA Aerospace Sciences Meeting, AIAA 2018-1807.. 2018 AIAA Aerospace Sciences Meeting. Orlando: AIAA.
• Meersman, J., & Hader, C. (2018, june). Meersman, J. A., Hader, C. & Fasel, H. F. Hypersonic boundary-layer transition: Comparison of the fundamental resonance breakdown for a flared and straight cone at Mach 6. 2018 Fluid Dynamics Conference, AIAA 2018-3851. AIAA 2018. Atlanta: AIAA.