NASA Langley Research Center Hampton, VA. Agenda Day 1 Mon., 24 July 2017
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1 NASA Langley Research Center Hampton, VA Agenda Day 1 Mon., 24 July 2017 Time Thrust Area Title PI 06:30-09:20 Registration 09:20-09:40 Welcome and Opening Remarks Ivett Leyva, AFOSR 09:40-10:30 SBLI - 3D 10:30-11:05 SBLI - 3D 3-D Shock/Turbulent BL Interaction Physics: Flow Morphology and System Dynamics through Imposed Disturbances Investigation of 3D Shock-Boundary Layer Interaction: A Combined Approach using Experiments, Numerical Simulations and Stability Analysis F. Alvi, FSU D. Gaitonde, OSU N. Clemens, U of TX R. Kumar, FSU B. Thurow, Auburn J. Little, U of AZ, H. Fasel, U of AZ A. Gross, NMSU 11:05-11:20 BREAK 11:20-11:55 SBLI -2D Flow Instability Analyses of Shock-Induced Separation Bubbles P. Martin, U of MD V. Theofilis, U of Liverpool 11:55-13:10 LUNCH 13:10-13:30 SBLI 13:30-13:50 SBLI 13:50-14:10 SBLI 14:10-14:35 SBLI The Effects of Strong Wall Cooling on Supersonic and Hypersonic Shock/boundary-Layer Interactions Inlet Isolator and Combustor Physics at Take-Over Region of Scramjet Engines (YIP) Investigation of Shock Boundary Layer Interactions to Unravel the Physics of Unstart in Axisymmetric Inlets Experimental Hypersonic SWBLI and Passive Hypersonic Transition Control J. Larsson, U of MD T. Lee, UIUC, V. Narayanaswamy, NCSU V. Narayanaswamy, NSCU A. Wagner, DLR Goettingen 14:35-14:50 BREAK 14:50-15:10 Elliptic Cone Studies (ECS) Measurement of Hypersonic Glide Vehicle Flow Fields R. Kimmel, AFRL/RQ Page 1
2 15:10-15:30 ECS 15:30-16:05 ECS Global Transient Growth Mechanisms in High-Speed Flows with Application to the Elliptic Cone Cross-flow Instability Receptivity to Environmental Disturbances at Hypersonic Speeds V. Theofilis, U of Liverpool R. Bowersox, TAMU H. Reed, TAMU 16:05-16:20 BREAK 16:20-16:40 Transition 16:40-17:00 Transition ONR - A Systematic Characterization of the Structure and Dynamics of Transitional Shock/boundary Layer Interactions ONR - Analysis and Simulations of the Structure and Dynamics of Transitional Shock/boundary Layer Interactions MEETING ADJOURN J. Schmisseur (ONR), U of TN G. Candler (ONR), U of MN Page 2
3 NASA Langley Research Center Hampton, VA Agenda Day 2 Tue., 25 July 2017 Time Thrust Area Title PI 07:30-8:00 BADGING & COFFEE 08:00-8:10 Opening Remarks Knox Millsaps, ONR 08:10-8:30 Transition 08:30-8:50 Transition 08:50-9:10 Transition Passive and Active Patterned Roughness for Cross-flow Transition Control at Mach 6 Laminar-to-turbulence Transition in Hypersonic B/L: Mode Interactions and Sensitivities to Mean-flow Non-linear Growth and Breakdown toward Turbulence in Hypersonic Boundary Layers T. Corke, U of ND T. McLaughlin, USAFA T. Zaki, JHU S. Girimaji, TAMU 09:10-9:25 BREAK 09:25-9:45 Transition 09:45-10:05 Transition 10:05-10:25 Transition 10:25-10:45 Transition (YIP) Numerical Simulation of Free-stream Acoustic Disturbances in Hypersonic Ground Facilities & Their Effect on BLT Hypersonic Transition Experiments in Ludweig Tubes (HBCU) The Effect of Multi-mode Induced Transition in a Hypersonic Boundary Layers Measurements of BL Instability and Transition in the M-6 Quiet Tunnel L. Duan, MUS&T (Rolla) Rolf Radespiel, TU of Braunschweig S. Smith, Howard U S. Schneider, Purdue U 10:45-12:00 LUNCH 12:00-12:20 Transition 12:20-12:40 Transition Direct Numerical Simulation of Hypersonic Transition Delay over Carbon/Carbon Ultrasonically Absorptive Coatings Nonlinear Transition Stages in Hypersonic Boundary Layers: Fundamental Physics, Transition Control and Receptivity C. Scalo, Purdue U H. Fasel, U of AZ 12:40-13:00 Transition A DNS Study on Hypersonic BL Receptivity X. Zhong, UCLA 13:00-13:20 Transition Plasma-Actuated Flow Control of Hypersonic Crossflow-Induced B/L Transition in a Quiet Tunnel T. Juliano, U of ND Page 3
4 13:20-13:35 BREAK 13:35-13:55 Transition 13:55-14:15 Transition Klebanoff Modes in Hiemenz Boundary Layer ONR - Towards a Mechanism-based Procedure for Predicting B/L Transition on Sender Models with Highly Swept Fins P. Ricco, The U of Sheffeld, UK S. Schneider, Purdue U 14:15-14:35 Transition ONR - Hypersonic Stability Predictions H. Reed, TAMU 14:35-14:50 BREAK 14:50-15:05 Transition 15:05-15:20 Transition 15:20-15:35 Transition 15:35-15:50 Transition 15:50-16:05 Transition 16:05-16:20 Transition 16:20-16:40 TM ONR - Predicting Hypersonic Laminar- Turbulent Transition with Direct Numerical Simulation ONR - Numerical Investigations of the Nonlinear Transition Stages in Hypersonic Boundary Layers for Navy Relevant Mach Numbers and Model Geometries/ Nonlinear Interaction Between First and Mack-mode Instabilities in High-Supersonic Flows ONR - Nonlinear Optimization in High-speed B/L: The most Unstable Nonlinear Disturbances & Robust Flow Design ONR - Adjoint methods for understanding distributed induced transition in hypersonic B/L ONR - Understanding hypersonic transition mechanisms through interactions between hydrodynamic, acoustic and thermal modes (YIP) The Influence of Multiple Interacting Primary Modes and Mode Representation on Hypersonic Boundary-layer Stability and Transition Prediction (YIP) Theoretical and Experimental Characterization of Turbulent Heat Transfer in Compressible Flows MEETING ADJOURN J. Poggie (new start), Purdue U H. Fasel,A. Craig (new start), U of AZ. T. Zaki (new start), JHU J. Nichols (new start/yip), U of MN D. Gaitonde (new start), OSU J. Kuehl, Baylor U M. Hultmark, Princeton U Page 4
5 NASA Langley Research Center Hampton, VA Agenda Day 3 Wed., 26 July 2017 Time Thrust Area Title PI 07:30-08:00 BADGING & COFFEE 08:00-08:25 Invited Speaker 08:25-08:55 FSI 08:55-09:30 FSI 09:30-09:50 FSI 09:50-10:10 FSI A Perspective on Computational Aerothermodynamics at NASA Characterization and Control of a Flap Undergoing Hypersonic FSI Developing an Experimental/Computational Methodology to Investigate the Response of Flexible Panels to Shockwaves Reduced Order Modeling for Hypersonic Aeroelasticity Direct Numerical Simulation of Compressible Turbulent Flows with Compliant Boundaries P. Gnoffo, NASA Langley A. Neely, UNSW, Australia S. Laurence, U of MD, D. Bodony, UIUC P. Tiso, ETH, Switzerland D. Bodony, UIUC 10:10-10:25 BREAK 10:25-10:45 DFI 10:45-11:05 DFI 11:05-11:25 DFI ONR - Advancing Transition Experiments in High Enthalpy Flows Investigating Sensor Characteristics for Scramjet Engine Control (STTR) Shear Sensors for High Speed, High Temperature Flow Applications J. Austin, Caltech K. Busa, J. Donbar, AFRL/RQ N. Hall, Silicon Audio 11:25-12:55 LUNCH/TOUR 12:55-13:15 DFI 13:15-13:35 DFI 13:35-13:55 DFI 13:55-14:15 DFI (YIP) Instantaneous Velocity Profiles of Wall- Bounded Shear Flows in Thermochemical Non-Equilibrium ONR - Hypervelocity Expansion Facility for Fundamental High-enthalpy Research ONR - Laminar Flow Control in Hypersonic Quiet Nozzle using Wall Suction: Feasibility Studies Femtosecond Laser Electronic Excitation Tagging (FLEET) for Quantitive Measurements in Turbulent Flows N. Parziale, Stevens Inst. Tech R. Bowersox, TAMU S. Schneider, Purdue U R. Miles, TAMU, Princeton Page 5
6 14:15-14:30 BREAK 14:30-14:50 NEE 14:50-15:25 NEE 15:25-15:45 NEE 15:45-16:05 NEE Non-equilibrium and Basic Energy Exchange Mechanisms in High Energy Flows Multi-Step Computational Modeling and Shock-Tube Study of Energy Transfer Processes in High-Enthalpy Air Mechanisms of Energy Transport in Gaseous Media Rapidly Expanding Non Equilibrium Hypersonic Flow 16:05-16:25 NEE Nonequilibrium Kinetics in High-Enthalpy Air 16:25-16:45 NEE Small-Molecule Reactions Relevant to the Hypersonic Flight Regime E. Josyula, AFRL/RQ I. Boyd, U of MI R. Hanson, Stanford G. Candler, U of MN R. Morgan, A. Veeraragavan, U of Queensland, Australia T. Schwartzentruber, G. Candler, D. Truhlar, U of MN Markus Meuwly, U of Basel MEETING ADJOURN Page 6
7 NASA Langley Research Center Hampton, VA Agenda Day 4 Thur., 27 July 2017 Time Thrust Area Title PI 07:30-08:00 BADGING & COFFEE 08:00-08:25 Invited Speaker 08:25-08:40 NEE 08:40-09:00 NEE Flight Experiment Verification of Shuttle Boundary Layer Transition Prediction Tool ONR -Real Gas Effects on Sound Radiation by Unstable Modes in Hypersonic B/L (YIP) Reduced-order Modeling Approach to Enable Kinetic Simulations of Nonequilibrium Hypersonic Flows 09:00-09:35 NEE Non-equilibrium Shock-shock and SBLI 09:35-09:55 NEE Validation of Models via Comparison with Data for Non-eq Hypersonic Flows S. Berry, NASA Langley A. Tumin, (new start), U of AZ M. Panesi, UIUC J. Austin, Caltech D. Levin, UIUC I. Wysong, AFRL/RQ 09:55-10:10 BREAK 10:10-10:25 TM 10:25-10:45 TM 10:45-11:05 TM 11:05-11:25 TM ONR - Aero-Thermo-Servo-Elastic analysis and optimization for high speed vehicles The Role of Kinetic Fluctuations in Laminar- Turbulent Transition of High-Speed Boundary-Layer Flows Resolvent analysis for compressible wall turbulence Physics Based Modeling of Compressible Turbulence D. Mavriplis (new start), U of Wyoming A. Tumin, U of AZ B. McKeon, Caltech P. Moin, Stanford U 11:25-12:55 LUNCH 12:55-13:20 TM 13:20-13:35 TM 13:35-13:50 TM Effects of wall curvature on hypersonic turbulent spatially-developing boundary layers ONR - Global stability and sensitivity analysis of a hypersonic slender cone (YIP) A Multiscale Morphing Continuum Analysis on Energy Cascade of Compressible Turbulence G. Araya, U of PR, K. Jansen, U of Co P. Moin (new start), Stanford U J Chen, Kansas State University Page 7
8 13:50-14:05 BREAK 14:04-14:20 Ablation 14:20-14:35 Ablation 14:35-15:15 Other 15:15-15:35 SBLI 15:35-16:15 Other BOLT (YIP) Fundamental Energy Transfer Mechanisms in High Temperature Phonon- Mediated Gas-Surface Interactions Nonequilibrium Gas-Surface Interactions at High Temperature (MURI) Integrated Measurement and Modeling Characterization of Stratospheric Turbulence Characterization of Secondary Flows in Turbulent Supersonic and Hypersonic Corners K. Stephani, UIUC T. Schwartentruber, G. Candler, U of MN T. Minton, MSU E. Corral, U of AZ J. Perepezko, U of WI Madison B. Argrow, U of CO, D. Fritts, Embry-Riddle Aero U, G. Candler, U of MN, D. Lawrence, U of CO, A. Muschinski, U of CO, A. Barjatva, Embry-Riddle Aero U J. Hofferth, N. Bisek, B. Rice, S. Peltier, B. Kocher, AFRL/RQ B. Wheaton, APL MEETING ADJOURN Page 8
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