• Environmental and Applied Fluid Dynamics

    To address revolutionary environmental and industrial challenges
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64th ESA Parabolic Flight Campaign Bulletin Board

The von Karman Institute is ready to participate to the 64th ESA Parabolic Flight Campaign which will take place from the 26th to the 29th April 2016.
The objectives of the VKI experiment is to determine both the liquid/gas interface shape and the fluid velocity during sloshing in a small cylindrical closed reservoir. During the parabolic flight test campaign the accelerations generated by the parabolic maneuver itself, will be used as trigger for a sloshing wave that will be therefore characterized.

This experiments at zero G was possible thanks to the contribution of ESA and BELSPO.

BELSPOESA

 

1. DURING THE FLIGHT

PIV sloshing in a small cylindrical closed reservoir

 

Liquid/gas interface shape and the fluid velocity during sloshing in a small cylindrical closed reservoir tested by the von Karman Institute (VKI) during the 64th ESA Parabolic Flight Campain (April 26-29, 2016).

 

 

Follow the zero G flight

2. BEFORE THE FLIGHT

Ready to fly
Ready to fly
Some hours before the flight
Some hours before the flight Laura Peveroni, Rosaria Vetrano and Alessia Simonini
25/05/2016
Laura Peveroni, Research Engineer at VKI and Alessia Simonini, PhD Candidate at VKI are aligning the laser
Testing the 1.8 g conditions 
22/04/2016
Sloshing in a VKI cup The laser

The motion of a free liquid surface inside its container is called sloshing and is strongly affected by the external excitations applied to the container. You may experience sloshing while walking with a cup of coffee in your hand with the inevitable consequent spilt.
The understanding and the prediction of this particular motion are extremely important in many fields. Indeed, the motion of liquids inside containers can refer to embarked tanks filled of fluid, motion of cooling liquids in systems subjected to earthquake or motion of propellant into reservoirs. The latter can influence the dynamic stability and performance of a vehicle, be it a ship, a missile, a rocket or a satellite.

 

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Faculty - EA

Delphine Laboureur

Associate Professor

Miguel Mendez

Associate Professor

Christophe Schram

Professor

Jeroen van Beeck

Dean of the Faculty and Head of the Department and Professor

  • Jean MULLER
  • Sara PORCHETTA (*)
  • Orkun TEMEL (*)
  • Alessandro ZARRI

*Collaborative Post Doc

  • Wassim ABDEL NOUR (*)
  • Muhsin Can AKKURT
  • Pierette ATIKPO (*)
  • Matija AVIROVIC (*)
  • David BARREIRO (*)
  • Bart BROUWERS (*)
  • Tommaso CARLESI
  • Adriana ENACHE
  • Loreline FAUGIER  (*)
  • Matilde FIORE
  • Domenico FIORINI
  • Benoît FOLOPPE
  • Erica GALLO
  • Emmanuel GILLYNS
  • Gert-Jan GLABEKE
  • Rui Pedro GONCALVEZ
  • Trond-Ola HAGBO  (*)
  • Yohanna HENROTEL  (*)
  • Tsvetelina IVANOVA
  • Baris KALE  (ITN)
  • Tom LAURIKS (*)
  • Aude LECARDONNEL
  • Rebeca MARINI  (*)
  • Pedro MARQUES
  • Abdelhafidh MOUMEN  (*)
  • Marcello NITTI  (*)
  • Carlo SANAPO
  • Fabio PINO
  • Romain POLETTI
  • Alexandros PALATOS-PLEXIDAS
  • Florentin PRUD'HOMME
  • Lorenzo SCHENA
  • Lorenzo VALLISA
  • Maxim VAN CAPPELLEN
  • Jan VAN DEN BERGHE
  • Adithya VEMURI
  • Kartik VENKATRAMAN

*Collaborative PhD

  • Konstantinos DIMITRIADIS
  • Pauline HAEZEBROUCK
  • Juliette KRUG
  • Francisco MONTEIRO
  • Efe ÖZTABAK
  • Manuel RATZ
  • Damien RIGUTTO
  • Jorge RODRIGUES
  • Berk SARIKAYA
  • Anilcan ULU
  • Umberto ZUCCHELLI

Project Office - Research Managers

Jean-Baptiste Gouriet

Research Manager

Philippe Planquart

Research Manager

Aude Lahalle

Research Manager