A full engine cycle analysis of a turbofan engine for optimum scheduling of variable guide vanes-Reference-Cited by-同舟云学术

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A full engine cycle analysis of a turbofan engine for optimum scheduling of variable guide vanes

Published:2015-12 Issue: Volume:47 Page:21-30
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Kim Sangjo^ORCID,Kim Donghyun,Son Changmin,Kim Kuisoon,Kim Myungho,Min Seongki

Funder

Agency for Defense Development

Ministry of Trade, Industry & Energy

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. The Jet Engine, Rolls-Royce plc;Rolls-Royce,2005

2. Plotting component maps in the Navy/NASA engine program (NNEP) – a method and its usage;Robert,1989

3. Survey on the mode transition technique in combined cycle propulsion systems;Huang;Aerosp. Sci. Technol.,2014

4. Combined cycle engine research in Japanese HYPR program;Miyagi,1998

5. Bypass flow pattern changes at turbo-ram transient operation of a combined cycle engine;Takata,2006

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