Conference Agenda

Nucleation barrier effect on pulsating heat pipe performance

Slaven Bajić¹, Guillaume Boudier¹, Eric Blondé², Typhaine Coquard², Vadim Nikolayev³

¹Centre National d'Études Spatiales (CNES), France; ²Airbus Defence and Space, Toulouse, France; ³Service de Physique de l’Etat Condensé, CEA, CNRS, Université Paris-Saclay, CEA Saclay, 91191 Gif-sur-Yvette Cedex, France

Experimental investigation of the evolution of an evaporating liquid film on a structured wall

Robin Maximilian Behle, Peter Stephan, Tatiana Gambaryan-Roisman

Technical University of Darmstadt

Flow Behavior in flow boiling experimental loop onboard the International Space Station

Osamu Kawanami¹, Hitoshi Asano², Koichi Inoue³, Ryoji Imai⁴, Koichi Suzuki⁵, Yasuhisa Shinmoto⁶, Satoshi Matsumoto⁷, Haruhiko Ohta⁸

¹University of Hyogo, Department of Mechanical Engineering, Himeji, Japan; ²Kobe University, Department of Mechanical Engineering, Kobe, Japan; ³The University of Kitakyushu, Department of Mechanical System Engineering, Kitakyushu, Japan; ⁴Muroran Institute of Technology, Department of Engineering, Muroran, Japan; ⁵Yamaguchi University of Science, Professor emeritus, Sanyo Onoda, Japan; ⁶Kyushu University, Department of Aeronautics and Astronautics, Fukuoka, Japan; ⁷Japan Aerospace Exploration Agency, Human Spaceflight Technology Directorate, Tsukuba, Japan; ⁸Kyushu University, Professor emeritus, Fukuoka, Japan

CONDENSATION HEAT TRANSFER AND FLOW CHARACTERISTICS IN A MINICHANNEL DURING A PARABOLIC FLIGHT CAMPAIGN

Arianna Berto¹, Nicolò Mattiuzzo¹, Alessandra Magnabosco¹, Marco Azzolin¹, Pascal Lavieille², Gaëtan Brunetto², Andrey Glushchuk³, Patrick Queeckers³, Stefano Bortolin¹, Marc Miscevic²

¹Department of Industrial Engineering, University of Padova, Padova, Italy; ²Université Paul Sabatier, Laboratoire Plasma et Conversion d’Energie, Toulouse, France; ³Universitè Libre de Bruxelles, Center for Research and Engineering in Space Technologies (CREST), Brussels, Belgium

Two-Phase Flow Experiments Onboard International Space Station - Analysis of liquid film structure of annular flow in adiabatic circular channel -

Hitoshi Asano¹, Osamu Kawanami², Koichi Inoue³, Ryoji Imai⁴, Yasuhisa Shinmoto⁵, Koichi Suzuki⁶, Satoshi Matsumoto⁷, Haruhiko Ohta⁸

¹Kobe University, Japan; ²University of Hyogo, Japan; ³The University of Kitakyushu, Japan; ⁴Muroran Institute of Technology, Japan; ⁵Kyushu University, Japan; ⁶Yamaguchi University of Science, Emeritus Professor, Japan; ⁷Japan Aerospace Exploration Agency (JAXA), Japan; ⁸Kyushu University, Emeritus Professor, Japan

Modeling Cryogenic Quenching Dynamics: Validation for Different Coating Thicknesses and Microstructures Features

Marco Graffiedi¹, Francis Dent², Sepideh Khodaparast², Matteo Bucci¹

¹Massachusetts Institute of Technology, United States of America; ²School of Mechanical Engineering, University of Leeds, UK