Numerical Investigation of Diffusers in Arc-Heated Wind Tunnel: Introducing a Novel and Efficient Hypersonic Diffuser-Reference-Cited by-同舟云学术

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Numerical Investigation of Diffusers in Arc-Heated Wind Tunnel: Introducing a Novel and Efficient Hypersonic Diffuser

Published:2022-09 Issue:5 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sol Baek Jin¹^ORCID,Choi Daesan¹^ORCID,Kim Kyu-Hong²^ORCID

Affiliation:

1. Ph.D. Candidate, Dept. of Mechanical and Aerospace Engineering, Seoul National Univ., Seoul 08826, Republic of Korea. ORCID: .

2. Professor, Dept. of Aerospace Engineering, Institute of Advanced Aerospace Technology, Seoul National Univ., Seoul 08826, Republic of Korea (corresponding author). ORCID: .

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/%28ASCE%29AS.1943-5525.0001469

Reference21 articles.

1. Aerothermodynamic analyses and redesign of GHIBLI Plasma Wind Tunnel hypersonic diffuser

2. Hypersonic and High-Temperature Gas Dynamics, Second Edition

3. Buscher, M., B. Esser, K. Kindler, and V. List. 1995. “Developments at the arc heated facility LBK of DLR.” In Vol. 367 of Aerothermodynamics for space vehicles, 357. Paris: European Space Agency.

4. Efficient diffuser design for plasma wind tunnels with a large blockage model

5. Numerical investigation of second throat exhaust diffuser performance with thrust optimized parabolic nozzles

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