Three-Dimensional Uncoupled Fluid Structure Analysis of Small Unmanned Aerial Vehicle Wing
Author:
Affiliation:
1. U.S. Army Research Laboratory, College Station, 77843 Texas
2. Texas A&M University, College Station, 77843 Texas
3. U.S. Army Research Laboratory, Aberdeen Proving Ground, 21005 Maryland
Funder
U.S. Department of Defense, U.S. Army, Combat Capabilities and Development Command, Army Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061921
Reference60 articles.
1. MODELING OF FLUID-STRUCTURE INTERACTION
2. Fluid-Structure Interaction
3. Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring
4. An experimental investigation on the aerodynamic performances of flexible membrane wings in flapping flight
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1. Aeroelastic Analysis of Adaptive Small Unmanned Aerial System Wings;AIAA SCITECH 2024 Forum;2024-01-04
2. Force/Moment-Conserving Pressure Mapping Scheme for Fluid/Structure Interaction Analysis;AIAA Journal;2023-04
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