Day 1 (30.3.2022)

14:30 – 14:50

Opening

Session 1:

14:50 – 15:35

15:40 – 16:00

Phenomena, structures, and mechanisms in high-speed flows with separation

Keynote 1: Pierre Dupont, Lionel Larchevêque and Jean-Paul Dussauge, Aix-Marseille Université, France

Tim Baur, Alessandro Accorinti, Sven Scharnowski, Christian J. Kähler, Institute of Fluid Mechanics and Aerodynamics, Bundeswehr University Munich, Neubiberg, Germany:
The Influence of Mach number, angle of attack and pitching Eigenfrequency on buffet(ing)

16:00 – 16:10

Coffee break

16:10 – 16:30

16:30 – 16:50

Andre Weiner, Richard Semaan, Institute of Fluid Mechanics, Technische Universität Braunschweig, Germany:
Simulation and modal analysis of transonic shock buffets on a NACA-0012 airfoil

R. D. Williams, Holger Babinsky, Engineering Department, University of Cambridge, UK:
Strip theory applied to corner effects in supersonic compression corner interactions

16:50 – 17:10

Plenary discussion and concluding remarks

Day 2 (31.3.2022)

Session 2:

13:30 – 14:15

14:20 – 14:40

Passive and active control strategies and methods

Keynote 2: Avraham Seifert, Tel Aviv University, Israel:
What is required for extending current active flow control capabilities to compressible flows?

C.Manisankar, Shashi Bhushan Verma, CSIR-National Aerospace Laboratories, Bangalore, India:
Off- and On-Surface Wake survey behind Vortex Generators Configurations at Mach 2.0

14:40 – 14:50

Coffee break

14:50 – 15:10

15:10 – 15:30

 15:30 – 15:45

Deepak P. Ramaswamy, Anne-Marie Schreyer, Institute of Aerodynamics, RWTH Aachen University, Germany:
Shock-induced flow separation control using air-jet vortex generators

S. B.Verma and C. Manisankar, Council of Scientific and Industrial Research (CSIR), National Aerospace Laboratories, Experimental Aerodynamics Division, Bangalore-560017, India:
Study of Surface Flow Topology with Variation in Spacing of Mechanical Vortex Generators in an Array

Plenary discussion 2

15:45 – 16:00

Coffee break

Session 3:

16:00 – 16:45

16:50 – 17:10

17:10 – 17:30

17:30 – 17:45

Physics of separation control

Keynote 3: Neil Sandham, University of Southampton, UK:
Implications of recent scale-resolving simulations for control of shock-induced unsteadiness

D. Gochenaur, R. Williams, K. Sabnis, and H. Babinsky, Engineering Department, University of Cambridge, UK:
The Effect of Streamwise Vortices on Compression Corner SBLIs

Robin Sebastian, Anne-Marie Schreyer, Institute of Aerodynamics, RWTH Aachen University, Germany:
A summary on the influence of different parametric variables on spanwise-inclined jet-injection in high-speed crossflows

Plenary discussion 3

17:45 – 17:50

Concluding remarks

Day 3 (1.4.2022)

Session 4:  

13:30 – 14:15

14:20 – 14:40

Potential of current control approaches to technical applications

Keynote 4: Marius Swoboda, Rolls-Royce, Germany

Ahmed H. Hanfy¹, Paweł Flaszyński², Piotr Kaczyński¹, ¹ Experimental Aerodynamics Department, ² Aerodynamics Department, Institute of Fluid-Flow Machinery, Polish Academy of Sciences (IMP PAN), Gdańsk, Poland: Roughness effect on shock wave boundary layer interaction on transonic fan profile

14:40 – 14:50

Coffee break

14:50 – 15:10

15:10 – 15:30

 
15:30 – 16:00

Lilia Hristozova, Robin Sebastian, Anne-Marie Schreyer, Institute of Aerodynamics, RWTH Aachen University, Germany:
Mechanical vortex generators in off-design conditions

Timothy Missing, Holger Babinsky, Engineering Department, University of Cambridge, UK:
Streamwise corner effects on oblique shock wave boundary layer interactions

Plenary discussion 4

16:00 – 16:15

Concluding remarks and closing