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Proceedings Papers

Heat Transfer Performance of Internal Cooling Turbine Blades Using Cutted-Root Rib Design

Cong-Truong Dinh, Tai-Duy Vu, Tan-Hung Dinh, Phi-Minh Nguyen
Proc. ASME. GT2020, Volume 7A: Heat Transfer, V07AT15A024, September 21–25, 2020
Paper No: GT2020-15389
https://doi.org/10.1115/GT2020-15389
View Paper titled, Heat Transfer Performance of Internal Cooling Turbine Blades Using Cutted-Root Rib Design
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Topics: Cooling, Design, Heat transfer, Turbine blades, Temperature, Computational fluid dynamics, Flow (Dynamics), Fluid dynamics, Gas turbines, Geometry
Journal Articles

Effects of Boot-Shaped Rib on Heat Transfer Characteristics of Internal Cooling Turbine Blades

Ky-Quang Pham, Quang-Hai Nguyen, Tai-Duy Vu, Cong-Truong Dinh
Journal: Journal of Heat Transfer
Article Type: Research-Article
J. Heat Transfer. October 2020, 142(10): 102106.
Paper No: HT-20-1042
https://doi.org/10.1115/1.4047490
Published Online: July 17, 2020
View Article titled, Effects of Boot-Shaped Rib on Heat Transfer Characteristics of Internal Cooling Turbine Blades
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Topics: Cooling, Flow (Dynamics), Heat transfer, Reynolds number, Turbine blades, Temperature
Proceedings Papers

Effects of a Circumferential Feed-Back Channel on Aerodynamic Performance of a Single-Stage Transonic Axial Compressor

Cong-Truong Dinh, Sang-Bum Ma, Kwang-Yong Kim
Proc. ASME. GT2017, Volume 2A: Turbomachinery, V02AT39A014, June 26–30, 2017
Paper No: GT2017-63536
https://doi.org/10.1115/GT2017-63536
View Paper titled, Effects of a Circumferential Feed-Back Channel on Aerodynamic Performance of a Single-Stage Transonic Axial Compressor
Open the PDF for Effects of a Circumferential Feed-Back Channel on Aerodynamic Performance of a Single-Stage Transonic Axial Compressor in another window
Topics: Compressors, Rotors, NASA, Navier-Stokes equations, Shapes