Numerical Study of Discrete Hole Supersonic Film Cooling with Shock Generator-Reference-Cited by-同舟云学术

Numerical Study of Discrete Hole Supersonic Film Cooling with Shock Generator

Published:2024-03 Issue:2 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhou Junfei¹,Zhang Yuqi²^ORCID,Xu Jinglei³^ORCID,Ding Haoyuan⁴

Affiliation:

1. Lecturer, State Key Laboratory of Mechanics and Control of Aeronautics and Astronautics Structures, School of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, PR China (corresponding author).

2. Postgraduate Researcher, State Key Laboratory of Mechanics and Control of Aeronautics and Astronautics Structures, School of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, PR China. ORCID: .

3. Professor, State Key Laboratory of Mechanics and Control of Aeronautics and Astronautics Structures, School of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, PR China. ORCID: .

4. Postgraduate Researcher, State Key Laboratory of Mechanics and Control of Aeronautics and Astronautics Structures, School of Energy and Power Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, PR China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5087

Reference62 articles.

1. Flow and Heat Transfer Predictions for Film Cooling

2. Film Cooling of Accelerated Flow in a Subscale Combustion Chamber

3. Experimental and Numerical Study of Supersonic Film Cooling

4. Bardina J. E. P. G. Huang and T. J. Coakly. 1997. “Turbulence modeling validation.” In Proc. 28th Fluid Dynamics Conf. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-2121.

5. Film-Cooling Effectiveness and Skin Friction in Hypersonic Turbulent Flow