figshare2026 · Astronomical catalogue
Data for Brachistochronous motion of a flat plate parallel to its surface immersed in a fluidThe dataset contains the solution of the mathematical problem presented in "Brachistochronous motion of a flat plate parallel to its surface immersed in a fluid". We determine the globally minimum time T needed to translate a thin submerged flat plate a given distance parallel to its surface within a work budget. The Reynolds number for the flow is assumed to be large so that the drag on the plate
Teesside University Research Data Repository2026 · dataset
Wing pitch timing and wing elevation modulate forces and body pitch in forward flapping flight - velocity fields 2This data set contains the velocity fields used in the analysis presented in the paper "Wing pitch timing and wing elevation modulate forces and body pitch in forward flapping flight". Each file gives the values of x, y, z, vx, vy, vz and mask at each point of a single sequence ; x,y,z is the position, vx,vy,vz are the velocity components and mask is the vorticity-based mask used in the reconstruc
Teesside University Research Data Repository2026 · dataset
Wing pitch timing and wing elevation modulate forces and body pitch in forward flapping flight - velocity fields 5This data set contains the velocity fields used in the analysis presented in the paper "Wing pitch timing and wing elevation modulate forces and body pitch in forward flapping flight". Each file gives the values of x, y, z, vx, vy, vz and mask at each point of a single sequence ; x,y,z is the position, vx,vy,vz are the velocity components and mask is the vorticity-based mask used in the reconstruc
Hugging Face Datasets2026 · Table · CSV
Aviation Propulsion-Aerodynamics Coupling Coherence Baseline Modeling v0.1What this dataset tests Whether a system can model the normal coupling between propulsion parameters and aerodynamic state. The signal is relationship shape and lag not threshold breaches. Required outputs coupling_coherence_index baseline_correlation_matrix phase_alignment_score stability_envelope lag_profile baseline_confidence Scoring conventions all scores range 0 to 1 stability envelope is a
Teesside University Research Data Repository2025 · dataset
ANÁLISE DO DESEMPENHO AERODINÂMICO DE ASAS EM FLUXO ESTACIONÁRIO UTILIZANDO O MÉTODO DE PAINÉISTrabalho apresentado ao III Simpósio Gaúcho de Engenharia Aeroespacial e Mecânica, Santa Maria, RS, Brasil.
e-cienciaDatos2025 · dataset · unknown
Dataset of "Advection-based multiframe iterative correction for pressure estimation from velocity fields"Dataset of the article: Chen, J., Raiola, M., & Discetti, S. (2025). Advection-based multiframe iterative correction for pressure estimation from velocity fields. Experimental Thermal and Fluid Science, 111407. The Advection-based Multiframe Iterative Correction (AMIC) is a space-time filter based on an advection function to filter the (Particle Image Velocimetry) PIV fields. The codes processing
Teesside University Research Data Repository2023 · dataset
Interspecies comparions of gliding animalsDataS3_Membrane.compare_July2023: Relative membrane area and gliding-related morphology of vertebrate gliders collected from literature.
Teesside University Research Data Repository2016 · dataset
Poster-1: Fluid-Structure Coupling of Membrane Wings for improved MAV PerformanceThe poster shows details about some results from my PhD, involving experimental wind tunnel measurements on bio-inspired flexible wings for small drones, UAVs and MAVs.
DataCite2014 · collection · unknown
CFD MODELING AND ANALYSIS OF ROTOR WAKE IN HOVER INTERACTING WITH A GROUND PLANEThe action of the rotor wake on loose sediment on the ground is primarily responsible for inducing the rotorcraft brownout phenomenon. Therefore, any simulation of brownout must be capable of accurately predicting the velocity field induced by the rotor when it is operating in ground effect. This work attempts to use a compressible, structured, overset Reynolds-Averaged Navier-Stokes (RANS) based