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Shuai Bi

Nanjing University of Aeronautics and Astronautics

Yudao Street

210016

Nanjing,, 210016

China

  • Nanjing University of Aeronautics and Astronautics

SCHOLARLY PAPERS

3

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105

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0

Scholarly Papers (3)

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1.

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

2.

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

3.

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