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Keynote and Invited Speakers

Gennaro CardoneGennaro Cardone

Professor, Dr.,
Chair of Aerospace Engineering Study Course
Università degli Studi di Napoli "Federico II", Italy
Department of Industrial Engineering –
Aerospace division


Thermo-fluid-dynamic analysis of innovative synthetic jet devices

Summary: Synthetic jets are largely used, especially in the field of electronic cooling; indeed their heat transfer performances have been widely investigated and some of the work performed at University of Naples Federico II is herein described. Heat transfer coefficients have been enhanced through the design of innovative synthetic jet devices; in particular, twin synthetic jets, multi orifice nozzles, chevron exit nozzles are considered. Obviously, the heat transfer performances of both the classic and innovative devices are strictly related to their impinging flow field on the surface to be cooled. In this work the behavior of innovative impinging synthetic jets is experimentally investigated by using Particle Image Velocimetry (PIV) and IR thermography leading to both time average and phase average flow velocity and heat transfer measurements. Three-dimensional coherent vortex structures, time-averaged and phase-averaged means, as well as turbulent statistics of flow fields and wall heat transfer data are presented and discussed.

Born in Naples (Italy) on 1963. Graduated in Mechanical Engineering with summa cum laude (1988). PhD in Aerospace Engineering (1991). Assistant professor (1992). Associate professor (1998). Actual position: Full Professor of Fluid Mechanics (2010) and Chair of the Aerospace engineering study courses, at the University of Naples Federico II, Department of industrial engineering, aerospace division. Scientific interests: two-beam and reference beam interferometry; velocimetry techniques such as PIV, Stereo-PIV and Tomo-PIV and their developments; heat transfer measurements with the infrared thermography technique, particularly focused on heat flux sensors and thermal image restoration; steady and unsteady natural convection; boundary layer diagnostics; transition detection and  flow field visualization from subsonic to hypersonic flow regimes; free and impinging synthetic jets; swirling jets; aerodynamic heating and its thermal visualization; thermal measurements in investment casting.
 


Victor V. KozlovVictor V. Kozlov

Professor, Dr.
Siberian branch of Russian academy of sciences
Khristianovich Institute of Theoretical and
Applied Mechanics, Russia
Novosibirsk State University, Russia


Visualization of conventional and combusting subsonic jet instabilities

Summary: Based on new information obtained for free microjets, this study is aimed to explain some phenomena of flame evolution at round and plane propane and hydrogen microjet combustion at presence of transverse acoustic field. It gives an overview of recent experimental results on instability and dynamics of jets at low Reynolds numbers and provides the recent advances in jet flow stability and combustion. Some clarification of the differences between top-hat and parabolic round and plane jet instability will also be given.

Education and academic degrees: Full Professor (Novosibirsk State University) 1992; DrSc (Academic Professor’s Thesis) 1987; Candidate's Degree (Ph.D.) in Physics and Math 1976; Masters degree, Novosibirsk State University, Russia 1969.

Work history: Khristianovich Institute of Theoretical and Applied Mechanics, Group leader of Aero-Physical Studies of Subsonic Flows, 1979-Present; Research fellow, 1969-1979.

Membership and assignments: Member of International Steering Committee of the 12th Asian Symposium on Visualization since 1994; Chairman and Organizer of the International workshop on the stability of homogeneous and heterogeneous fluids flows, Novosibirsk, since1997; Member of Scientific Committee of International Conference on Methods of Aerophysical Research (ICMAR), Novosibirsk, Russia, since 1998; Chairman and Organizer of the IUTAM Symposium on Separating Flow and Jets, Novosibirsk, 1990; Member of Scientific Committee of the 5th IUTAM Symposium on Laminar-Turbulent Transition, 1999, Sedona Arizona, Toulouse, France, 1989; Member of Scientific Committee of the IUTAM Symposium on Mechanics of Passive and Flow Control, 1998, Göttingen, Germany; others.

Awards: The Silver Zsukovskij Medal for great contribution to the Aviation Theory from Russian Academy of Sciences, 1993; The Petrov Medal for the contribution to the Hydrodinamic Instability, 2008. The Sedov Medal for the contribution in the field of fluid mechanics, 2015.


WIlliam SaricWilliam Saric

Distinguished Professor of Aerospace Engineering
George Eppright '26 Chair in Engineering
Texas A&M University
Aerospace Engineering


Flight experiments on discrete roughness element technology for laminar flow control

William S. Saric has been Professor of Aerospace Engineering at Texas A&M University since January 2005. He received his PhD in Mechanics from the Illinois Institute of Technology in 1968 and has held appointments at Sandia Laboratories (Atomic and Fluid Physics, 1963-1966, 1968-1975), Virginia Polytechnic Institute and State University (Engineering Science and Mechanics, 1975-1984), Tohoku University, Japan (Aeronautics and Astronautics, 1991-1992), and Arizona State University (Mechanical and Aerospace Engineering, 1984-2005).

He is a registered Professional Engineer in Virginia and was an Aerospace Engineering Evaluator for ABET.

He is a Fellow of AIAA, APS, and ASME. He received the AIAA Fluid Dynamics Award in 2003, the G.I. Taylor Medal from SES in 1993, the Scientific Achievement Award from AGARD (NATO) in 1996, and the Alumni Research Award from V.P.I.&S.U in 1984. In 2006, he was elected to the National Academy of Engineering for “contributions to the fundamental understanding and control of shear-flow and boundary-layer transition”.

He has established two major wind tunnel research facilities and a flight research center at Texas A&M University and was the Director of the AFOSR/NASA National Center for Hypersonic Laminar-Turbulent Transition Research.

Most recently, he has conducted experimental, and flight research on stability, transition, and control of two-dimensional and three-dimensional boundary layers for subsonic aircraft, supersonic aircraft and reentry vehicle applications.

Invited Speakers

Prof. Mo Samimy
The Ohio State University, USA
Title: Active Flow Control in High-Speed Flows

Session: Flow/Fluid Control

Dr. Li-Hao Feng
Beihang University, Beijing, China
Title: Active control of bluff body wake using synthetic jets.

Session: Flow/Fluid Control. Special Recognition: Young Researcher

Dr. Campbell Carter
Air Force Research Laboratory, USA
Title: Advances in KHz Imaging Diagnostics for Practical Problems.

Session: Measurements

Prof. Stanislav Gordeyev
University of Notre Dame, USA
Title: Aero-Optical Effects to Study Flow Dynamics at Hypersonic Speeds.

Session: Measurements

Prof. Shinichiro Ito
Kogakuin University, Japan
Title: Memories of Prof. Nakayama and Dedicated presentation to Prof. Nakayama, “PIV analysis and aerodynamic vibration on the soccer ball wake.”

Session: Visualization

Prof. Jan Stasiek
Gdansk University of Technology, Poland
Title: Liquid Crystals, PIV and IR-Photography in Selected Technical and Biomedical Applications.

Session: Visualization

Dr. Christopher Limbach
Texas A&M University, USA
Title: Visualization and Applications of Femtosecond, Nanosecond and Dual-Pulsed Laser-Induced Plasmas.

Session: Visualization. Special Recognition: Young Researcher

Dr. Nicolas Benard
University of Poitiers, France
Title: Linear surface plasma actuator, a useful device for manipulation of coherent vortices in turbulent flows.

Session: ND Workshop

Prof. Thomas Corke
University of Notre Dame, USA
Title: TBD.

Session: ND Workshop

Dr. Pavel Georgievsky
Institute of Mechanics MSU, Moscow, Russia
Title: Thermal Spike Conception for Supersonic Flow Control and Wave Drag Reduction of Bodies.

Session: ND Workshop

Dr. Marios Kotsonis
Delft University of Technology, Netherland
Title: Towards control of swept wing transition using plasma actuators.

Session: ND Workshop

Prof. Jonathan Poggie
Purdue University, USA
Title: Controlling Compressible, Turbulent Flow with Plasmas: A Review.

Session: ND Workshop

Dr. Andrey Starikovsky
Princeton University, USA
Title: Dynamic Stall Control at High Angle of Attack by NS Pulsed Actuator.

Session: ND Workshop