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- W2016200386 abstract "Vibrational characteristics of a model of NASA's GAW-2 airfoil are studied computationally and experimentally. The computational procedures are based on the Finite Element Method. The experimental procedures are based on the Laser Hologram Interferometry methods; more specifically, the methods of stroboscopic Heterodyne Hologram Interferometry and time- average Electro-Optic Holography are used. Comparison of the computational results with the experimental results shows good correlation." @default.
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- W2016200386 modified "2023-09-23" @default.
- W2016200386 title "<title>Holographic study of vibrations of a wing section</title>" @default.
- W2016200386 doi "https://doi.org/10.1117/12.140796" @default.
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