Cong-Truong Dinh
Cong-Truong Dinh
Lecturer, Aeronautical and Space Engineering Department, Hanoi University of Science and Technology
Verified email at hust.edu.vn - Homepage
Title
Cited by
Cited by
Year
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
282015
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
172017
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
112017
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 (3), 599-611, 2020
52020
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
42019
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), 034111, 2020
32020
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
32020
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
22021
Effects of Stator Shroud Injection on the Aerodynamic Performance of a Single-Stage Transonic Axial Compressor
CT Dinh, SB Ma, KY Kim
Transactions of the Korean Society of Mechanical Engineers B 41 (1), 9-19, 2017
22017
Parametric study of casing groove combined with blade tip injection and ejection in a transonic axial compressor
CT Dinh, KY Kim
Asian Congress on Gas Turbines, 2014
22014
Recirculation-groove coupled casing treatment for a transonic axial compressor
TD Vuong, KY Kim, CT Dinh
Aerospace Science and Technology 111, 106556, 2021
12021
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
12020
Effect of air bleeding on aerodynamic performance of a single-stage axial compressor
CT Dinh, KY Kim
유체기계 연구개발 발표회 논문집, 343-344, 2016
12016
Effects of Air Injection on Aerodynamic Performance of a Single-Stage Transonic Axial Compressor
CT DINH, KY KIM
1
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), 076104, 2021
2021
Effect of Two-Head Flared Hole on Film Cooling Performance over a Flat Plate
XT Le, DA Nguyen, CT Dinh, QH Nguyen
Aerospace 8 (5), 128, 2021
2021
Aerodynamic Performance of an Annular Combustion Chamber Cooling with Swirler Design
CT Dinh, XT Le, TN Hoang, QA Pham
International Journal of Fluid Machinery and Systems 14 (1), 1-12, 2021
2021
Effects of stator splitter blades on aerodynamic performance of a single-stage transonic axial compressor
KQ Pham, XT Le, CT Dinh
Journal of Mechanical Engineering and Sciences 14 (4), 7369-7378, 2020
2020
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, 1-14, 2020
2020
Heat Transfer Performance of Internal Cooling Turbine Blades Using Cutted-Root Rib Design
CT Dinh, TD Vu, TH Dinh, PM Nguyen
Turbo Expo: Power for Land, Sea, and Air 84164, V07AT15A024, 2020
2020
The system can't perform the operation now. Try again later.
Articles 1–20