default author photo

Chen Xia

Nanjing University of Aeronautics and Astronautics

SCHOLARLY PAPERS

4

DOWNLOADS

106

TOTAL CITATIONS

1

Scholarly Papers (4)

Actions:
Email selected abstracts
1.

Aerodynamic Design of Fixed-Wing Vtol Aircraft Powered by Gas-Driven Fan Propulsion System

Number of pages: 32 Posted: 25 Dec 2024
Yuanzhao Zhu, Guoping Huang, Chen Xia and Yang Wu
Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics and Nanjing University of Aeronautics and Astronautics
Downloads 47 (1,170,409)
Citation 1

Abstract:

Loading...

Vertical Takeoff and Landing (VTOL)Aerodynamic CowlGas-Driven Thrust Fan (GDTF)Subsonic Aircraft DesignCFD Simulation

2.

Numerical Investigation of Highly Loaded Tandem Blades for High Subsonic Flow

Number of pages: 27 Posted: 05 Dec 2024
Yuanzhao Zhu, Guoping Huang and Chen Xia
Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics and Nanjing University of Aeronautics and Astronautics
Downloads 20 (1,448,301)

Abstract:

Loading...

gas-driven thrust fan, inlet guide vane, tandem blade, highly loaded, gap geometry, induced circulation

3.

Effects of Tip Clearance Height on Hot-Streak Migration in High Subsonic Micro Turbine

Number of pages: 15 Posted: 08 Sep 2022
Jingde Zhu, Xin Xiang, Xiaoan Hu and Chen Xia
Nanchang Hangkong University, Nanchang Hangkong University, Nanchang Hangkong University and Nanjing University of Aeronautics and Astronautics
Downloads 20 (1,448,301)

Abstract:

Loading...

Micro Axial Turbine, Hot Streak, Blade Tip Clearance, Leakage Flow, Numerical simulation

4.

Numerical study of highly loaded tandem blades for high subsonic flow

Number of pages: 27 Posted: 14 Oct 2025
Yuanzhao Zhu, Guoping Huang, Chen Xia and Yang Wu
Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics and Nanjing University of Aeronautics and Astronautics
Downloads 19 (1,470,786)

Abstract:

Loading...

Inlet guide vane, Tandem blades, Gap geometry optimization, Aerodynamic interactions, Boundary layer control., Integrated intake system