Digital Image Correlation (DIC) for Aircraft GVT

DIC pattern on aircraft during GVT

The goal of a ground vibration test (GVT) is to experimentally characterize the structural resonances of an aircraft. This is an important step in the aircraft certification process as it helps to validate the models used for aeroelastic prediction and to verify that no flutter occurs within the flight envelope.

Challenges in aircraft instrumentation during GVT

Instrumenting the aircraft for this test can be a tedious task. Hundreds of sensors – single- and multi-axis accelerometers – must be attached to the aircraft structure to measure the vibration response to the shaker excitation. These sensors must be placed at well-defined locations on the structure and positioned with the right orientation to allow accurate measurements which requires care and time. They should be properly glued to the structure to avoid that they detach during the test which would lead to inaccurate results or delays in the measurement campaign.

Modern data acquisition systems provide advanced capabilities for accelerating the instrumentation phase and for verifying that the measurement set-up is correct. But still, engineering teams involved in the GVT are often under pressure to deliver results as quickly as possible to minimize delays in the aircraft program. And the measurement task might be quite complex, involving multiple aircraft configurations to be tested and requiring to capture all relevant phenomena affecting the aircraft structural response. For instance, characterizing non-linearities in the aircraft structure might require detailed investigations and extra instrumentation. This challenges the GVT teams to deliver results which are complete, accurate and within time.

Ground vibration tests involve complex instrumentation with hundreds of sensors on the aircraft structure

Looking for more flexible measurement techniques

Although accelerometers have been the most used sensors in past GVT campaigns, they only provide discrete data, involve lengthy instrumentation and require careful cabling management. One may wonder if a contactless measurement technique could be used to solve these challenges and complement accelerometer-based measurements.

Digital image correlation set-up used during aircraft GVT: speckle pattern applied on the structure (left) and digital cameras positioned around the aircraft (right).

Getting deeper insights into aircraft structural dynamics with Digital Image Correlation

Imagine using your camera to film the GVT test and directly obtain the vibration of the aircraft structure out of this movie. Well, this is pretty much what the Digital Image Correlation technique (DIC) allows to do! This contactless measurement technique relies on digital cameras and provides full-field vibration data by processing the sequence of acquired images. Originally used for material testing and quasi-static measurements, the technique was further developed to be applied to dynamic measurements and modal testing. As opposed to accelerometers or vibrometer measurements providing discrete results, this DIC technique directly provides full-field displacement information.

Moreover, the camera set-up time is fairly quick and the calibration process very easy. A speckle pattern must be applied on the structure to ensure that the images captured by the cameras can be processed and provide displacement information. Multiple synchronized cameras can be used to cover large measurement surfaces. This makes it possible to use the DIC technique for aircraft vibration measurements.

The technique has been applied here on an F16 aircraft during GVT and combined with accelerometer measurements.  Global modes information of the complete aircraft obtained with accelerometers is combined with detailed results from DIC on specific part of the structure. This allows to focus on areas of the aircraft structure such as the wing tip where non-linearities might be observed.


The measurement system allows full synchronization between the digital cameras, the measured accelerometer data and the shaker excitation signals. This enables to process the combined data in a streamlined way. Frequency response functions and modal parameters are calculated the same way on both data sets. In that sense the DIC technique is really complementary to traditional accelerometer-based measurement approach.

The DIC technique does not necessarily require high-speed cameras to measure vibrations and characterize the modal behavior of the aircraft. More affordable low-speed cameras can also be used. In this case, a resampling technique is automatically applied after the measurement which allows to extract vibration data at frequencies well above the frame rate of the cameras.

The DIC technique offers interesting capabilities to accelerate the modal testing of aerospace structures and get deeper insights into structural dynamics of complete aircraft during GVT. This technique can nicely complement traditional accelerometer-based measurements and help testing teams being more efficient.

To learn more about the DIC technique, read this article.

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