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5 results for “FSI”

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zenodo36/100

Vertical temperature profiles obtained from Venus Express and Akatsuki radio occultation data using FSI

<p>Vertical temperature profiles of Venusian atmosphere obtained from selected radio occultation data taken in ESA&#39;s Venus Express and JAXA&#39;s Akatsuki missions. The temperatures were retrieved using a radio holographic method, Full Spectrum Inversion (FSI). The data list and format are given in two Excel files and the data are given in text files with an extension &quot;.dat&quot;.</p>

opencc-by-4.0Mar 2021View details →
zenodo36/100

Data set for bionic simulation of double clap-and-fling wing mechanism with SPH FSI method

<p>Data set containing the rigid-body based flapping wing models coupled with smoothed particle hydrodynamics (SPH), by means of <a href="https://github.com/DualSPHysics/DualSPHysics/wiki/9.-New-in-DualSPHysics#new-in-dualsphysics-v50">DualSPHysics version 5.0 </a>and <a href="https://projectchrono.org/download/">Project Chrono</a>.</p><p>These models are part of the paper:</p><blockquote><p>Yanwei Zhang, Zhonglai Wang, Saullo G. P. Castro. Bionic simulation of double clap-and-fling wing mechanism with SPH FSI method. EngXriv Preprint, 2022. <a href="https://doi.org/10.31224/2652">DOI: 10.31224/2652</a></p></blockquote><p>File "simulations.zip" contains the simulation files.</p><p>File "DualSPHysics_v5.0.zip" contains the compiled DualSPHysics software.</p><p>Procedure to run the simulations on a Windows machine:</p><ul><li>Working directory: .\simulations\flappingwing\case01</li><li>Step 1: Obtain rigid bodies by modeling of SOLIDWORKS and Macro command of FreeCAD (e.g. external_wing111.stl)</li><li>Step 2: Run ".bat" file (e.g. flapping01.bat) to start simulation and force acquisition</li><li>Step 3: Revise ".bat" and ".xml" (e.g. flapping01.bat and flapping01_Def.xml)to adapt to the next case. If required, change the model and Macro command of step 1. Common modification items:</li></ul><p>&lt;geometry&gt;-&lt;definition&gt; &lt;floatings&gt;- &lt;floating&gt;&lt;angularvel&gt; &lt;floatings&gt;- &lt;floating&gt;&lt;property&gt; &lt;properties&gt;-&lt;propertyfile&gt; &lt;initials&gt; &lt;execution&gt;-&lt;special&gt;-&lt;chrono&gt; &lt;execution&gt;-&lt;special&gt;-&lt;inout&gt; &lt;parameters&gt;&nbsp;</p><ul><li>Step 4: Run "Filter.m" to handle force data by filters. Step 5: Compare forces of all cases. PS: Other files are revised function files derived from DualSPHysics 5.0.</li></ul><p>&nbsp;</p><p>Abstract: Three-dimensional numerical simulations of flexible flapping wings based<br>on the fluid-structure interaction in biological and bioinspired flow have become a<br>vibrant and challenging research topic. The present paper focuses on a parametric<br>study of the aerodynamic performance of a bionic flexible clapping wing. The proposed<br>model deforms the wing in spanwise and chordwise directions based on the six rigid<br>bodies connected along the wing veins using ball links and springs. Unsteady effects of<br>flapping wing micro air vehicles with a double clap-fling configuration are investigated<br>using an air-solid interaction model based on smoothed particle hydrodynamics and<br>rigid multi-body dynamics. A validation experiment determined the convergence<br>conditions and computational model accuracy. The proposed numerical model is<br>evaluated in terms of flexible variation law and aerodynamic performance. The results<br>indicate that the flapping frequency, angle of attack, and wind velocity significantly<br>influence the lift. Furthermore, increasing the frequency will monotonically expand<br>the maximum and time-averaged lift curve values. When the angle of attack is less<br>than 30 ◦, the influence on the time-averaged and maximum lift is proportional to the<br>angle of attack. When the angle of attack is larger than 45 ◦, a stall-like condition<br>is detected. To broaden the applicability of the present findings, a dimensionless<br>parameter, reduced frequency, is defined, and its influence on the maximum and time-<br>averaged lift is investigated. This parametric study shows that as the reduced frequency<br>increases, the maximum and time-averaged lift increases and then decreases. The<br>present study could reach a modeling framework that better explains the clapping<br>wing aerodynamics.<br>&nbsp;</p>

opencc-by-4.0Oct 2022View details →
zenodo32/100

FSI-ROM-Predictor-Data

Open the record for dataset details and reuse information.

openOct 2024View details →
ClinicalTrials.gov32/100

Pilot Feasibility Trial of the Family Strengthening Intervention in Rwanda (FSI-R)

ClinicalTrials.gov study NCT01509573. IPD Sharing: Not stated. Countries: 1. Publications: 23.

restrictedIPD-UNDECIDEDFeb 2026View details →
ClinicalTrials.gov24/100

Study of GS-0189 (Formerly FSI-189) as Monotherapy and in Combination With Rituximab in Participants With Relapsed/Refractory Non-Hodgkin Lymphoma

ClinicalTrials.gov study NCT04502706. IPD Sharing: NO. Countries: 1. Publications: 0.

closedIPD-NOFeb 2026View details →

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International Brain Laboratory public data

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Last verified 2026-04-29Open record