Modal Parameter Extraction via Propeller-Driven Vibration Testing
Gabriele Dessena, Alessandro Pontillo

TL;DR
This paper evaluates Propeller-driven Vibration Testing (PVT) as a cost-effective, output-only alternative to Ground Vibration Testing for aircraft, demonstrating its ability to reliably extract low-frequency modal parameters under various excitation conditions.
Contribution
It introduces PVT as a novel, practical approach for modal analysis in aircraft structures, utilizing the Natural Excitation Technique with the Loewner Framework for data interpretation.
Findings
Propeller excitation maintains dominant resonances in spectra.
Low-throttle conditions introduce masking harmonics.
PVT reliably identifies modal parameters with high repeatability.
Abstract
Ground Vibration Testing (GVT) supports aircraft certification but often requires lengthy and costly campaigns. Propeller-driven Vibration Testing (PVT) is assessed here as an output-only alternative, in line with Operational Modal Analysis approaches such as Taxi Vibration Testing and Flight Vibration Testing. A cantilever Aluminium 7075-T6 wing spar is instrumented with seven accelerometers and excited by an outboard electric motor and propeller. Seven runs are carried out: a motor-off baseline, five constant-throttle cases, and a manual up-down throttle sweep. The acquired spectra indicate that the dominant resonances remain observable under propeller excitation, while low-throttle conditions introduce narrowband harmonics that may mask structural peaks; the sweep reduces persistent overlap. Modal parameters are identified for the baseline and sweep cases using the Natural Excitation…
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Taxonomy
TopicsVehicle Noise and Vibration Control · Aeroelasticity and Vibration Control · Structural Health Monitoring Techniques
