Full name: Dinh Cong Truong
Title: Title
Date of birth: 1976
Position: Lecturer, Aeronautical and Space Engineering
Tel: 09.3463.8035
E-mail: truong.dinhcong@hust.edu.vn, truongdc.ite@gmail.com
1. Courses taught
2. Fields of interest
3. Education
| Degree | Year | Field and university |
| Doctor | 2017 | Mechanical Engineering in Aircraft Propulsion, Inha University, Incheon, Korea |
| Master of research | 2007 | Aerodynamic and Aeroacoustic in Aeronautic, University of Paris 6, France. |
| Master of research | 2007 | Energetic, Propulsion and Aerospace, University of Paris 10, France. |
| Master of Professional | 2007 | Energetic, Propulsion and Aerospace, University of Paris 10, France. |
| Master of research | 2001 | Modelisation and Computation in Mechanics of Continuum, Inter-university cooperation program between Liege University, Belgium and Hanoi University of Science and Technology, Vietnam. |
| Engineering | 1999 | Aeronautical Engineering, Hanoi University of Science and Technology, Hanoi, Vietnam |
4. Brief research background and working experiences
2013-2017: Ph.D. Student at Inha University, Incheon, Korea.
2018-present: Lecturer at Aeronautical and Space Engineering Department, Hanoi University of Science and Technology, Hanoi, Vietnam
5. Remarkable scientific projects
04/2014 – 03/2017, Aerodynamic-Structural Design Optimization of Wide Chord Fan, HANWHA Techwin, KOREA. Position: member.
6. Patents
1. Cong-Truong Dinh and Kwang-Yong Kim. Single-stage transonic axial compressor with stator injector. Korean Patent Certification No. 10-1724361. April 2017.
2. Cong-Truong Dinh and Kwang-Yong Kim. Stator partial span splitter blades with single-stage transonic axial compressor. Korean Patent Certification No. 10-1799071. November 2017.
7. Một số bài báo điển hình
[1] Cong-Truong Dinh, Sang-Bum MA and Kwang-Yong Kim, Aerodynamic Optimization of a Single-Stage Axial Compressor with Stator Shroud Air Injection, AIAA journal, Vol. 55, No. 8, August 2017. IF: 1.638.
[2] Cong-Truong Dinh and Kwang-Yong Kim, Effects of Non-Axisymmetric Casing Grooves Combined with Airflow Injection on Stability Enhancement of an Axial Compressor, International Journal of Turbo & Jet-Engines. IF: 0.47.
[3] Cong-Truong Dinh, Man-Woong Heo and Kwang-Yong Kim, Aerodynamic performance of transonic axial compressor with a casing groove combined with blade tip injection and ejection, Aerospace Science and Technology Vol 46, pp. 176–187, 2015. IF: 2.151.
[4] Cong-Truong Dinh, Sang-Bum MA and Kwang-Yong Kim, Effects of Stator Shroud Injection on the Aerodynamic Performance of a Single-Stage Transonic Axial Compressor, Trans. Korean Soc. Mech. Eng. B, Vol. 41, No. 1, pp. 9~19, 2017.
[5] Cong-Truong DINH and Kwang-Yong KIM, Effects of a Circumferential Feed-Back Channel on Aerodynamic Performance of a Single-Stage Transonic Axial Compressor, Proceedings ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition, GT2017-63536, June 27-29, 2017, Charlotte, NC USA.
[6] Cong-Truong DINH and Kwang-Yong KIM, Effect of Air Bleeding on Aerodynamic Performance of a Single-Stage Axial Compressor, 2016 한국유체기계학회 동계 학술대회 논문집 여수 디오션리조트, 2016. 11. 30~12. 02.
[7] Cong-Truong DINH and Kwang-Yong KIM, Effects of Air Injection on Aerodynamic Performance of a Single-Stage Transonic Axial Compressor, ICESEEI ’16: Applications of Engineering in Renewable Energy Sources, 73208-127, Barcelona, Spain, February 13-15, 2016.
[8] Cong-Truong DINH and Kwang-Yong KIM, Effects Of Partial-Span Splitter Blades Combined With Air Injection on Aeodynamic Performance of a Single-Stage Transonic Axial Compressor, Proceedings of 7th International Symposium on Fluid Machinery and Fluids Engineering 18th – 22th October, 2016, Lotte City Hotel, Jeju, Korea.
[9] Cong-Truong DINH and Kwang-Yong KIM, Effects of Air Injection on Aerodynamic Performance of Single-Stage Transonic Axial Compressor, ASME Turbo Expo 2016, 13-17 June, 2016, Seoul, Korea.
[10] Cong-Truong DINH and Kwang-Yong KIM, Aerodynamic Performance of a Single-Stage Axial Compressor using Stator Splitter Blades combined with Airflow Injection, 한국유체기계학회 동계 학술대회 논문집 롯데시티호텔, 제주, 2015. 12. 02~04.
[11] Cong-Truong DINH and Kwang-Yong KIM, Performance Analysis of a Transonic Axial Compressor using Slot Casing Grooves and Blade Tip Injection, The 13th Asian International Conference on Fluid Machinery, AICFM13-015, 7th – 10th September 2015, Tokyo, Japan.
[12] Cong-Truong DINH and Kwang-Yong KIM, Effects of Airflow Injection and Ejection in a Casing Groove on Aerodynamic Performances of a Transonic Axial Compressor, Proceeding of ACFD10, The 10th Asian Computational Fluid Dynamics Conference, ACFD10-65, October 19-23, 2014, Jeju, Korea.
[13] Cong-Truong DINH and Kwang-Yong KIM, Parametric Design Study of Casing Groove combined with Blade Tip Injection and Ejection on Aerodynamic Performance of a Transonic Axial Compressor, Asian Congress on Gas Turbines 2014 (Acgt 2014), ACGT2014-0038, August 18-20, 2014, Seoul, Korea.
[14] Cong Truong Dinh and Jea-Woon Kim, Analysis of Turbulent Flow Structures and Aerodynamic Noise on Side View Mirrors of a Vehicle, ISFMFE 2012, 5th International Symposium on Fluid Machinery and Fluids Engineering, 24-27 October 2012, Lotte Hotel, Jeju, Korea.
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