Prediction of axial compressor blade excitation by using a two-way staggered fluid-structure interaction model.

MLA

Brandsen, Jacobus D., et al. “Prediction of Axial Compressor Blade Excitation by Using a Two-Way Staggered Fluid-Structure Interaction Model.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 232, no. 8, June 2018, pp. 1495–514. EBSCOhost, https://doi.org/10.1177/0954410017694056.

APA

Brandsen, J. D., van der Spuy, S. J., & Venter, G. (2018). Prediction of axial compressor blade excitation by using a two-way staggered fluid-structure interaction model. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 232(8), 1495–1514. https://doi.org/10.1177/0954410017694056

Chicago

Brandsen, Jacobus D., Sybrand J. van der Spuy, and Gerhard Venter. 2018. “Prediction of Axial Compressor Blade Excitation by Using a Two-Way Staggered Fluid-Structure Interaction Model.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232 (8): 1495–1514. doi:10.1177/0954410017694056.