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http://dx.doi.org/10.5139/JKSAS.2008.36.4.321

Design/Construction and Performance Test of Hypersonic Shock Tunnel Part Ⅰ: Design Method of Hypersonic Shock Tunnel  

Lee, Bok-Jik (서울대학교 기계항공공학부 대학원)
Lee, Hyoung-Jin (서울대학교 기계항공공학부 대학원)
Kim, Sei-Hwan (서울대학교 기계항공공학부 대학원)
Jeung, In-Seuck (서울대학교 기계항공공학부 항공우주 신기술 연구소)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.36, no.4, 2008 , pp. 321-327 More about this Journal
Abstract
The shock tunnel as a hypersonic ground test facility was designed, constructed and its performance test was conducted to reproduce the high speed flow which the hypersonic propulsion system is encountered. The design points were understood and the conceptual design was completed using the quasi one dimensional operation analysis code. After that, the specific performance and compartment design were completed using CFD simulation as the part analysis. The facility was then constructed according to those design results and the performance test was conducted for various operation conditions. In this paper, we suggested the design method of hypersonic shock tunnel including the conceptual and performance design using theoretical analysis and the quasi 1D Multi-species computational fluid dynamics code.
Keywords
Hypersonic Propulsion System; Shock Tunnel;
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