Complete Dataset for Journal of Fluids and Structures publication:
"Near-wake characteristics of rigid and membrane wings in ground effect" (2018) by, R.Bleischwitz, R.de Kat, B.Ganapathisubramani
Written 01-04-2018
by Robert Bleischwitz (robert.bleischwitz@gmail.com) General Comments 0.) This specific upload contains the full timeresolved dataset of the JFS-paper (~27GB of timeresolved MATLAB files) 1.) The attached time-resolved-data relates to experimental windtunnel measurements on passive membrane wings for MAVs. The data was aquired between 2012-2016 at the University of Southampton, involving Robert Bleischwitz as PhD student, who was supervised by Roeland de Kat and Bharathram Ganapathisubramani. 2.) The attached data is given time-resolved and time-synchronised at 800Hz over a imaging-period of 5000 images, involving load measurements via a 6-axis load-cell ATI Nano17 /25N, deformation measurements via Digitial Image Processing (high-speed DIC) and stereo flow measurements via two high-speed cameras (high-speed stereo PIV). 3.) More setup and processing details can be found in the paper "Near-wake characteristics of rigid and membrane wings in ground effect" (2018) by the authors R. Bleischwitz, R. de Kat, B. Ganapathisubramani
Published in: -Journal of Fluids and Structures: https://doi.org/10.1016/j.jfluidstructs.2018.03.007 - University of Southampton: http://doi.org/10.5258/SOTON/D0461 4.) All load/deformation/flow folders contain a README.txt(Use 1st) and Instructions.m (Use 2nd) MATLAB-file, which give further supporting details how to illustrate the time-resolved-data 5.) This specific upload contains the full time-resolved dataset, including: -Cases: a.) Rigid and Membrane wings b.) Height of ground(from trailing edge, in referecne to chord length): h/c=2, 0.25 and 0.1 c.) Angle-of-attack: 10,15,25deg d.) DATA available (Timeresolved and time-synchronised): -Loads in high speed (10 kHz) -Membrane deformations in high speed(800Hz) -Stereo Flow velocities in wake at high-speed (800Hz) Abstract of Journal-publication:
Wind tunnel measurements are conducted at a Reynolds numbers of Re = 56,000 to examine the characteristics of
near-wake vortices of rigid flat-plates and membrane wings from free-flight into ground–effect conditions. Synchronised
high-speed load cell measurements, digital image correlation and particle image velocimetry are performed to
resolve lift, drag and ...
Written 01-04-2018
by Robert Bleischwitz (robert.bleischwitz@gmail.com) General Comments 0.) This specific upload contains the full timeresolved dataset of the JFS-paper (~27GB of timeresolved MATLAB files) 1.) The attached time-resolved-data relates to experimental windtunnel measurements on passive membrane wings for MAVs. The data was aquired between 2012-2016 at the University of Southampton, involving Robert Bleischwitz as PhD student, who was supervised by Roeland de Kat and Bharathram Ganapathisubramani. 2.) The attached data is given time-resolved and time-synchronised at 800Hz over a imaging-period of 5000 images, involving load measurements via a 6-axis load-cell ATI Nano17 /25N, deformation measurements via Digitial Image Processing (high-speed DIC) and stereo flow measurements via two high-speed cameras (high-speed stereo PIV). 3.) More setup and processing details can be found in the paper "Near-wake characteristics of rigid and membrane wings in ground effect" (2018) by the authors R. Bleischwitz, R. de Kat, B. Ganapathisubramani
Published in: -Journal of Fluids and Structures: https://doi.org/10.1016/j.jfluidstructs.2018.03.007 - University of Southampton: http://doi.org/10.5258/SOTON/D0461 4.) All load/deformation/flow folders contain a README.txt(Use 1st) and Instructions.m (Use 2nd) MATLAB-file, which give further supporting details how to illustrate the time-resolved-data 5.) This specific upload contains the full time-resolved dataset, including: -Cases: a.) Rigid and Membrane wings b.) Height of ground(from trailing edge, in referecne to chord length): h/c=2, 0.25 and 0.1 c.) Angle-of-attack: 10,15,25deg d.) DATA available (Timeresolved and time-synchronised): -Loads in high speed (10 kHz) -Membrane deformations in high speed(800Hz) -Stereo Flow velocities in wake at high-speed (800Hz) Abstract of Journal-publication:
Wind tunnel measurements are conducted at a Reynolds numbers of Re = 56,000 to examine the characteristics of
near-wake vortices of rigid flat-plates and membrane wings from free-flight into ground–effect conditions. Synchronised
high-speed load cell measurements, digital image correlation and particle image velocimetry are performed to
resolve lift, drag and ...