Testing and Prediction of Heat Exchanger Performance for Liquid Propulsion Engine Based on Simulation Experiment-Reference-Cited by-同舟云学术

Testing and Prediction of Heat Exchanger Performance for Liquid Propulsion Engine Based on Simulation Experiment

Published:2023-12-19 Issue: Volume: Page:
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Shin Min Kyu,Oh Jeong Hwa,Cha Jeong Yeol,Ko Young Sung^ORCID,Yu I Sang

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42405-023-00694-1.pdf

Reference12 articles.

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3. Park JS, Yu IS, Shin MK, Oh JH, Lee HJ, Ko YS (2019) Numerical study on performance characteristics of exhaust gas properties in channel and coil type heat exchanger. Trans Korean Soc Mech Eng B 43:1–9. https://doi.org/10.3795/KSME-B.2019.43.1.001

4. Yu IS, Shin DH, Oh JH, Shin MK, Lee HJ, Ko YS (2019) Design/construction/operation of experimental apparatus for performance evaluation of heat exchanger. Trans Korean Soc Mech Eng B 43:313–321. https://doi.org/10.3795/KSME-B.2019.43.5.313

5. Shin DS, Kim KS, Han SY, Bang JS, Kim HY, Jo DH (2017) Conceptual design of turbine exhaust system for 3rd stage of launch vehicle. In: Proceedings of the Korean society of propulsion engineers spring conference, pp 1068–1071