Boundary Layers

Large-scale PIV measurements of the boundary layer beneath a towed structure

E. Uksul(1), A. Laskari(1), S. Schreier(2), C. Poelma(1)

1: Dept. of Process & Energy, Delft University of Technology, The Netherlands
2: Dept. of Maritime and Transport Technology, Delft University of Technology, The Netherlands

Near-wall 3D Lagrangian particle tracking over a 6:1 prolate spheroid

Y. Sawalhi, C. Fort, M.J. Yamakaitis, P.M. Bardet

Dept. of Mechanical and Aerospace Engineering, The George Washington University, Washington D.C., United States

Volumetric Lagrangian Particle Tracking in high Reynolds number pipe flow

D. Schanz(1), R. Geisler(1), J. Lemarechal(1), L. Lazzarini(2), G. Bellani(2), A. Talamelli(2), S.T. Thoroddsen(3), V. Mugundhan(3), A. Alhareth(3,4), K.R. Dharmarajan(3), A. Aguirre-Pablo(3), R. Deshpande(5), H. Nagib(6), A. Schröder(1,7)

1: German Aerospace Center (DLR), Institute of Aerodynamics and Flow Technology, Göttingen, Germany
2: Department of Industrial Engineering / CIRI Aerospace, University of Bologna, Forlì, Italy
3: King Abdullah University of Science and Technology (KAUST), Saudi Arabia
4: King Abdulaziz City for Science and Technology (KACST), Riyadh 12354, Saudi Arabia
5: School of Engineering, RMIT University, Melbourne 3000 VIC, Australia
6: Illinois Tech, Chicago, USA
7: Brandenburg University of Technology, Chair of Image Based Measurement Techniques, Cottbus, Germany

Experimental study of three-dimensional turbulent boundary layers in a simplified wing-body junction

A. Weingärtner, B. Ganapathisubramani

Department of Aeronautical and Astronautical Engineering, University of Southampton, United Kingdom

Vortex distribution and interaction within a perturbed turbulent boundary layer

R. Ribeiro, E.K. Longmire, M.A. Green

Aerospace Engineering and Mechanics, University of Minnesota, USA

Geometry Effect of Streamwise Finlet on Manipulating Wall-Pressure Fluctuations

Z. Pan, Q. Ye

State Key Laboratory of Fluid Power and Mechatronic Systems, Department of Mechanics, Zhejiang University, Hangzhou 310027, China

Drag Reduction Of Turbulent Boundary Layer Over Air-Fed Superhydrophobic Structured Surface

Qiwei Zhang

School of Engineering Science, University of Chinese Academy of Sciences, Beijing, China

LDA-FFID coupled measurements of two-height canopy flow in a wind tunnel

V. Babin(1), L. Shig(2), A. Liberzon(2), Y. Bohbot-Raviv(1)

1: Environmental Wind Tunnel Laboratory, Israel Institute for Biological Research, POB 19, Ness Ziona 7410001, Israel
2: School of Mechanical Engineering, Tel Aviv University, POB 39040, Tel Aviv 6997801, Israel

Turbulent boundary layer under a transient change in pressure gradients

K. Zheng, D.W. Carlson, B. Ganapathisubramani

Dept. of Aeronautical and Astronautical Engineering, The University of Southampton, UK

Cross-Plane Particle Concentration Measurements in a Simulated Atmospheric Turbulent Boundary Layer

A. Sankaran, R. Hain, C.J. Kähler

University of the Bundeswehr Munich Institute of Fluid Mechanics and Aerodynamics 85577 Neubiberg, Germany

Hypersonic Boundary Layer Velocimetry During Transpiration Cooling Using NO-LIF Imaging

Tianshu Wu (1), Xin Li (2), Jiwei Li (2), Yejun Wang (2), Qiu Wang (2), Yutao Huo (1), Wei Zhao (2)

1. China University of Mining and Technology, Xuzhou, China
2. Institute of Mechanics, Chinese Academy of Sciences, Beijing, China