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Evaluation of the compressive response of notched composite panels using a full-field displacement measurement system
1999
40th Structures, Structural Dynamics, and Materials Conference and Exhibit
unpublished
An experimental and analytical evaluation of the compressive response of two composite, notched stiffened panels representative of primary composite wing structure is presented. A three-dimensional full-field image correlation technique is used to measure all three displacement components over global and local areas of the test panels. Point-wise and full-field results obtained using the image correlation technique are presented and compared to experimental results and analytical results
doi:10.2514/6.1999-1406
fatcat:yxllzvncabeqpao64bfn7lk3mi