Low-Pressure Hydrogen Jets from a Single Hole Injector Investigated With 2D Raman and Schlieren Imaging

B. Rüppel(1,2), B. Lehnert(1,2), S. Rieß(1,2), E. Berrocal(2,3), M. Wensing(1,2)

1: Friedrich-Alexander-Universität Erlangen-Nürnberg (FAU), Professorship for Fluid Systems Technology, Cauerstraße 4, 91058 Erlangen, Germany
2: FAU, Erlangen Graduate School in Advanced Optical Technologies (SAOT), Konrad-Zuse-Straße 3-5, 91052 Erlangen, Germany
3: Division of Combustion Physics, Department of Physics, Lund University, P.O. Box 118, SE-22100 Lund, Sweden

The impact of swirl on a starting vortex from an impulse jet identified in PIV data

A. Sarkhosh, J. Ren, D.S. Nobes

Department of Mechanical Engineering, University of Alberta, Canada

Flow Characteristics in Rectangular and Circular Containers with Air Injected from a Slit Nozzle

T. KIWATA(1), R. ASAI(2), K. ARIMA(2), Y. KAWAMURA(3), H. UCHIDA(3), K. TOYODA(4)

1: School of Mechanical Engineering, Kanazawa University, Ishikawa, Japan
2: Graduate School of Natural Science and Technology, Kanazawa University, Ishikawa, Japan
3: ALTEMIRA Can Co., Ltd., Shizuoka, Japan
4: Hokkaido University of Science, Hokkaido, Japan

Experimental Analysis of Submerged and Plunging Turbulent Jets with Air Entrainment

M.T. Migliorino, F. Acquaviva, S. Marcocci, G. Moscato, G.P. Romano

Department of Mechanical and Aerospace Engineering, Sapienza University of Rome, via Eudossiana 18, 00184, Rome, Italy

Evolution of turbulent kinetic energy and dissipation rate in near and far field region of a single jet using PIV

K. Ghamkhar, S. Puttinger, M. Weiß, M. Saeedipour

Department of Particulate Flow Modelling, Johannes Kepler University Linz, Austria

Flow Characterisation of Highly Integrated High-Aspect-Ratio Rectangular Nozzle

F. De Gregorio(1), M. Inverno(1), L. Lazzarini(2), A. Talamelli(2), R. Camussi(3), K.S. Rossignol(4)

1 CIRA, Italian Aerospace Research Centre, Capua, Italy
2 Department of Industrial Engineering / CIRI Aerospace, University of Bologna, Italy
3 Engineering Department, University of Roma Tre, Italy
4 DLR, German Aerospace Center, Braunschweig, Germany

Local cluster-based identification of flow dynamics

Q.L. Li-Hu, G.Y.C. Maceda, A. Ianiro, S. Discetti

Dept. of Aerospace Engineering, Universidad Carlos III de Madrid, Spain

Identification and characterization of a starting vortex from initiation within a confined tube

J. Ren, A. Sarkhosh, D.S. Nobes

Department of Mechanical Engineering, University of Alberta, Canada

Meandering-driven flapping of a flexible flag in a turbulent free-surface water jet

M. Sollevanti, G.P. Romano

Dept. of Mechanical and Aerospace Engineering, University “La Sapienza”, Rome, Italy