Mathematical modeling and characteristic analysis for over-under turbine based combined cycle engine-Reference-Cited by-同舟云学术

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Mathematical modeling and characteristic analysis for over-under turbine based combined cycle engine

Published:2018-07 Issue: Volume:148 Page:141-152
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ma Jingxue,Chang Juntao,Ma Jicheng,Bao Wen,Yu Daren

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference33 articles.

1. Revolutionary Turbine Accelerator (RTA) Demonstrator, AIAA Paper;McNelis,2005

2. The GE-NASA RTA Hyperburner Design and Development, NASA/TM;Lee,2005

3. Revolutionary Turbine Accelerator (RTA) Two-Stage-to-Orbit (TSTO) Vehicle Study, AIAA Paper;Bradley,2002

4. Combined Cycle Engine Research in Japanese HYPR Project, AIAA Paper;Miyagi,1995

5. ACES Sӓnger-type TSTO Family with Common First Stage, AIAA Paper;Hendrick,1998

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