Measurements of Panel Vibration with DIC and LDV Imaged Through a Mach 5 Flow
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Publisher
Springer Nature Switzerland
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-34910-2_5
Reference14 articles.
1. Ehrhardt, D.A., Allen, M.S., Yang, S., Beberniss, T.J.: Full-field linear and nonlinear measurements using continuous-scan laser Doppler vibrometry and high speed three-dimensional digital image correlation. Mech. Syst. Signal Process. 86, 82–97 (2017). Full-field, non-contact vibration measurement methods: comparisons and applications. https://doi.org/10.1016/j.ymssp.2015.12.003
2. Spottswood, S.M., Beberniss, T.J., Eason, T.G., Perez, R.A., Donbar, J.M., Ehrhardt, D.A., Riley, Z.B.: Exploring the response of a thin, flexible panel to shock-turbulent boundary-layer interactions. J. Sound Vib. 443, 74–89 (2019). https://doi.org/10.1016/j.jsv.2018.11.035
3. Brouwer, K.R., Perez, R.A., Beberniss, T.J., Spottswood, S.M., Ehrhardt, D.A., Wiebe, R.: Investigation of aeroelastic instabilities for a thin panel in turbulent flow. Nonlinear Dyn. 104, 3323–3346 (2021). https://doi.org/10.1007/s11071-021-06571-4
4. Eitner, M.A., Ahn, Y.-J., Vanstone, L., Musta, M.N., Sirohi, J., Clemens, N.: Effect of shock-wave boundary layer interaction on vibratory response of compliant panel. AIAA paper 2021-2493, AVIATION 2021 Forum (2021). https://doi.org/10.2514/6.2021-2493
5. Varigonda, S.V., Jenquin, C., Narayanaswamy, V.: Impact of panel vibrations on the dynamic field properties in supersonic flow. AIAA paper 2021-2926, Aviation 2021 Forum (2021). https://doi.org/10.2514/6.2021-2926
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