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http://dx.doi.org/10.6108/KSPE.2015.19.6.033

Design Study of a Dual-Mode Ramjet Engine with Large Backward-Facing Step  

Yang, Inyoung (Engine System Research Team, Korea Aerospace Research Institute)
Lee, Yang-Ji (Engine System Research Team, Korea Aerospace Research Institute)
Lee, Kyung-Jae (Engine System Research Team, Korea Aerospace Research Institute)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.19, no.6, 2015 , pp. 33-41 More about this Journal
Abstract
Scaled model of a dual-mode ramjet engine with large backward-facing step, as a component of the rocket-based combined cycle engine, was designed. Design parameters were derived for this engine with the consideration of application for the rocket-based combined cycle engine. Design methodology was established for these design parameters. The design was partially verified through numerical study. Flow characteristics of the dual-mode ramjet engine with large backward-facing step was investigated experimentally. The design methodology for relevant design parameters established in this study was verified as feasible.
Keywords
Scramjet Engine; Dual-Mode Ramjet Engine; Rocket-Based Combined Cycle; Backward-Facing Step; Hypersonic Wind Tunnel;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
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