Near-wall, Reynolds-stress model calculations of transonic flow configurations relevant to aircraft aerodynamics

MLA

Jakirlić, Suad, et al. “Near-Wall, Reynolds-Stress Model Calculations of Transonic Flow Configurations Relevant to Aircraft Aerodynamics.” International Journal of Heat & Fluid Flow, vol. 28, no. 4, Aug. 2007, pp. 602–15. EBSCOhost, https://doi.org/10.1016/j.ijheatfluidflow.2007.04.001.

APA

Jakirlić, S., Eisfeld, B., Jester-zürker, R., & Kroll, N. (2007). Near-wall, Reynolds-stress model calculations of transonic flow configurations relevant to aircraft aerodynamics. International Journal of Heat & Fluid Flow, 28(4), 602–615. https://doi.org/10.1016/j.ijheatfluidflow.2007.04.001

Chicago

Jakirlić, Suad, Bernhard Eisfeld, Roland Jester-zürker, and Norbert Kroll. 2007. “Near-Wall, Reynolds-Stress Model Calculations of Transonic Flow Configurations Relevant to Aircraft Aerodynamics.” International Journal of Heat & Fluid Flow 28 (4): 602–15. doi:10.1016/j.ijheatfluidflow.2007.04.001.