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Modal Parameters Evaluation in a Full-Scale Aircraft Demonstrator under Different Environmental Conditions Using HS
Ángel Jesús Molina-Viedma1, Elías López-Alba2, Luis Felipe-Sesé3
1Departamento de Ingeniería Mecánica y Minera, Campus Las Lagunillas, Universidad de Jaén, 23071 Jaén, Spain. ajmolina@ujaen.es.
This study introduces a non-invasive method using 3D digital image correlation for aircraft fuselage modal analysis. This technique accurately captures structural vibrations and modal parameters for improved cabin noise control.
Area of Science:
- Mechanical Engineering
- Aerospace Engineering
- Structural Dynamics
Background:
- Aircraft cabin noise impacts passenger comfort and crew performance.
- Effective noise and vibration control require accurate structural analysis.
- Traditional sensors for modal analysis are invasive and limit spatial resolution.
Purpose of the Study:
- To present a non-invasive methodology for experimental modal characterization of aircraft structures.
- To assess the structural response using high-speed 3D digital image correlation.
- To evaluate the impact of cabin pressurization and structural modifications on modal parameters.
Main Methods:
- Utilized high-speed 3D digital image correlation for full-field, non-invasive measurements.
- Performed experimental modal analysis on a full-scale front fuselage demonstrator.
- Excited the structure with an electrodynamic shaker and analyzed time-domain displacements.
Main Results:
- Identified natural frequencies and full-field operational deflection shapes.
- Characterized dynamic response patterns without perturbing the structure.
- Assessed changes in modal parameters due to cabin pressurization and local modifications.
Conclusions:
- The 3D digital image correlation methodology provides accurate modal characterization.
- This non-invasive technique complements traditional methods like accelerometers.
- The findings contribute to enhanced aircraft cabin noise and vibration control strategies.
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