Theo dõi
Cong-Truong Dinh
Cong-Truong Dinh
Email được xác minh tại hust.edu.vn - Trang chủ
Tiêu đề
Trích dẫn bởi
Trích dẫn bởi
Năm
Aerodynamic performance of transonic axial compressor with a casing groove combined with blade tip injection and ejection
CT Dinh, MW Heo, KY Kim
Aerospace Science and Technology 46, 176-187, 2015
512015
Numerical investigation of truncated-root rib on heat transfer performance of internal cooling turbine blades
CT Dinh, TM Nguyen, TD Vu, SG Park, QH Nguyen
Physics of Fluids 33 (7), 2021
422021
Large eddy simulation of the turbulence heat and mass transfer of pulsating flow in a V-sharp corrugated channel
TT Hoang, CT Dinh, F Plourde
International Journal of Heat and Mass Transfer 166, 120720, 2021
342021
Recirculation-groove coupled casing treatment for a transonic axial compressor
TD Vuong, KY Kim, CT Dinh
Aerospace Science and Technology 111, 106556, 2021
332021
Numerical investigation of heat transfer characteristics of pin-fins with roughed endwalls in gas turbine blade internal cooling channels
KDC Do, DH Chung, DQ Tran, CT Dinh, QH Nguyen, KY Kim
International Journal of Heat and Mass Transfer 195, 123125, 2022
292022
Aerodynamic optimization of a single-stage axial compressor with stator shroud air injection
CT Dinh, SB Ma, KY Kim
AIAA journal 55 (8), 2739-2754, 2017
282017
Effects of a circumferential feed-back channel on aerodynamic performance of a single-stage transonic axial compressor
CT Dinh, SB Ma, KY Kim
Turbo Expo: Power for Land, Sea, and Air 50787, V02AT39A014, 2017
272017
Effects of rotor-bleeding airflow on aerodynamic and structural performances of a single-stage transonic axial compressor
CT Dinh, DQ Vu, KY Kim
International Journal of Aeronautical and Space Sciences 21, 599-611, 2020
262020
Numerical aero-thermal study of high-pressure turbine nozzle guide vane: Effects of inflow conditions
HM Phan, PH Duan, CT Dinh
Physics of Fluids 32 (3), 2020
232020
Heat transfer enhancement by a pair of asymmetric flexible vortex generators and thermal performance prediction using machine learning algorithms
MS Kang, SG Park, CT Dinh
International Journal of Heat and Mass Transfer 200, 123518, 2023
202023
Effects of boot-shaped rib on heat transfer characteristics of internal cooling turbine blades
KQ Pham, QH Nguyen, TD Vu, CT Dinh
Journal of Heat Transfer 142 (10), 102106, 2020
172020
Wind power forecasting based on hourly wind speed data in South Korea using machine learning algorithms
J Kim, A Afzal, HG Kim, CT Dinh, SG Park
Journal of Mechanical Science and Technology 36 (12), 6107-6113, 2022
162022
Effects of non-axisymmetric casing grooves combined with airflow injection on stability enhancement of an axial compressor
CT Dinh, KY Kim
International Journal of Turbo & Jet-Engines 36 (3), 283-296, 2019
132019
Effects of Pin-Fins with Trapezoidal Endwall on Heat Transfer Characteristics in Gas Turbine Blade Internal Cooling Channels
CT Dinh, KDC Do, DH Chung, HS Truong
Journal of Mechanical Science and Technology 37 (5), 1-12, 2023
112023
Aeromechanic performance of a single-stage transonic axial compressor with recirculation-bleeding channels
CT Dinh, TD Vuong, XT Le, TM Nguyen, QH Nguyen
Australian Journal of Mechanical Engineering 21 (1), 154-167, 2020
102020
Aerodynamic and structural performances of a single-stage transonic axial compressor with blade fillet radius
HQ Chu, CT Dinh
International Journal of Intelligent Unmanned Systems, 2022
92022
Parametric study on aerodynamic performance of a single-stage transonic axial compressor with recirculation-bleeding channels
KQ Pham, QH Nguyen, TD Vuong, CT Dinh
International Journal of Fluid Machinery and Systems 13 (2), 348-360, 2020
82020
Aerodynamic performance optimization of a single-stage axial compressor using circumferential bleeding airflow
DQ Tran, XT Le, VH Nguyen, CT Dinh, TS Vu
Journal of Aeronautics, Astronautics and Aviation 54 (4), 451-466, 2022
72022
AERODYNAMIC PERFORMANCES OF A SINGLE- STAGE TRANSONIC AXIAL COMPRESSOR USING AN INCLINED CASING GROOVE
AT Nguyen, HD Vo, CT Dinh, HQ Chu
Australian Journal of Mechanical Engineering, 2022
62022
Numerical investigation of the flows and heat transfer characteristics of internal cooling channels with separated ribs in gas turbine blades
VH Nguyen, TD Vu, CT Dinh, SG Park
Physics of Fluids 36 (3), 2024
52024
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