UH-60A Rotor Structural Loads Analysis with Fixed System Structural Dynamics Modeling
Author:
Affiliation:
1. U.S. Army Aviation Development Directorate, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C035102
Reference17 articles.
1. Rotor Airloads Prediction Using Loose Aerodynamic/Structural Coupling
2. Review of Rotor Loads Prediction with the Emergence of Rotorcraft CFD
3. Application of Computational Fluid Dynamics/Computational Structural Dynamics Coupling for Analysis of Rotorcraft Airloads and Blade Loads in Maneuvering Flight
4. Rotor Loads Prediction on the ONERA 7A Rotor Using Loose Fluid/Structure Coupling
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1. Quantification of Rotorcraft Blade Dynamic Inertial Imbalance;AIAA AVIATION 2022 Forum;2022-06-20
2. UH-60A Airloads Workshop-Setting the Stage for the Rotorcraft CFD/CSD Revolution, Part II: Ongoing Progress, Impact, and Lessons Learned;J AM HELICOPTER SOC;2022
3. UH-60A Airloads Workshop—Setting the Stage for the Rotorcraft CFD/CSD Revolution, Part II: Ongoing Progress, Impact, and Lessons Learned;Journal of the American Helicopter Society;2022-04-01
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