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Junkui Mao

Nanjing University of Aeronautics and Astronautics

Yudao Street

210016

Nanjing,, 210016

China

  • Nanjing University of Aeronautics and Astronautics

SCHOLARLY PAPERS

7

DOWNLOADS

272

TOTAL CITATIONS

0

Scholarly Papers (7)

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1.

Performance evaluation and transient characteristics of a kerosene-fueled SOFC-GT hybrid aviation power system for long-endurance UAVs under multi-scenario operation

Downloads 71 (933,592)

Performance evaluation and transient characteristics of a kerosene-fueled SOFC-GT hybrid aviation power system for long-endurance UAVs under multi-scenario operation

Number of pages: 33 Posted: 06 Jan 2026
Xinyong Jiang, Fengli Liang, Junkui Mao, Shuang Liang, Le Kang and Lingzhi Han
Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics, 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 55 (1,083,731)

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SOFC, UVA, Long-endurance, Multi-scenario operation, Dynamic performance

Performance evaluation and transient characteristics of a kerosene-fueled SOFC-GT hybrid aviation power system for long-endurance UAVs under multi-scenario operation

Number of pages: 60 Posted: 23 Apr 2026
Xinyong Jiang, Fengli Liang, Junkui Mao, Shuang Lian, Le Kang and Lingzhi Han
Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics, 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 16 (1,579,999)

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SOFC, UVA, Long-endurance, Multi-scenario operation, Dynamic performance

2.

Thermal-Oxidation Coupled Analysis Method for Unidirectional Fiber-Reinforced C/Sic Composites in Air Oxidizing Environments Below 1000 °C

Number of pages: 24 Posted: 12 Sep 2022
Chenwei Zhao, Zecan Tu and Junkui Mao
Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics and Nanjing University of Aeronautics and Astronautics
Downloads 49 (1,074,648)

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C/SiC composites, oxidation, Thermal conductivity, thermal model

3.

Effect of Multiple Ribs and Tip Injection on the Aerothermal Characteristics of the Squealer Tip in Turbine Stage

Number of pages: 24 Posted: 13 Jun 2022
Shuai Bi, Junkui Mao, Pingting Chen, Feng Han and Lei Wang
Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics and affiliation not provided to SSRN
Downloads 47 (1,097,529)

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gas turbine, Squealer Tip, Tip injection, Heat Transfer, Multi-cavity, Numerical Simulation

4.

The Multiscale Thermal Analysis of 2.5d Woven Ceramic Matrix Composites Turbine Vane Considering the Mesoscale Structures

Number of pages: 21 Posted: 21 Aug 2023
Zecan Tu, Chenwei Zhao, Junkui Mao, Ailing Zhu and Xuan Liang
Nanjing University of Aeronautics and Astronautics, 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 33 (1,290,922)

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ceramic matrix composite, woven structure, thermal analysis, multiscale method, mesoscale model

5.

Coupled Effects of Typical Thermodynamic Parameters On the Flow and Heat Transfer in a High-Pressure Turbine Outer Ring with Impingement-Film Composite Cooling Structure

Number of pages: 33 Posted: 09 Oct 2023
Longfei Wang, Chengliang Lv, Junkui Mao, Ziqiang Li, Dewei Zhang and Shuai Bi
Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics, 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 30 (1,345,526)

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Impingement-film cooling structure, Cooling performance, Coupled effect, Working condition parameters

6.

Influence Mechanism of Impingement and Film on the Flow and Heat Transfer of Turbine Outer Ring with Composite Cooling Structure Under Different Operating Parameters

Number of pages: 34 Posted: 17 Oct 2023
Longfei Wang, Chengliang Lv, Junkui Mao, Ziqiang Li, Dewei Zhang and Shuai Bi
Nanjing University of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics, 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 28 (1,345,526)

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Impingement-film composite cooling, film cooling, Turbine outer ring, Working conditions, Cooling effectiveness

7.

Experimental Study on Transient Heat Transfer Characteristics of Ceramic Matrix Composite Plates with High Temperature Air Oxidation

Number of pages: 21 Posted: 01 May 2025
Chenwei Zhao, Zecan Tu, Xinyu Lan, Junkui Mao and Haiyang Zhao
Nanjing University of Aeronautics and Astronautics, 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 14 (1,518,554)

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ceramic matrix composite, transient heat transfer, high temperature oxidation, heat convection experiment