APA (7th ed.) Citation

Kahveci, H. S., Haldeman, C. W., Mathison, R. M., & Dunn, M. G. (2013). Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine--Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall. Journal of Turbomachinery, 135(2), 1. https://doi.org/10.1115/1.4006776

Chicago Style (17th ed.) Citation

Kahveci, Harika S., Charles W. Haldeman, Randall M. Mathison, and Michael G. Dunn. "Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine--Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall." Journal of Turbomachinery 135, no. 2 (2013): 1. https://doi.org/10.1115/1.4006776.

MLA (9th ed.) Citation

Kahveci, Harika S., et al. "Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine--Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall." Journal of Turbomachinery, vol. 135, no. 2, 2013, p. 1, https://doi.org/10.1115/1.4006776.