Operation matching model and analysis between an air inlet and a compressor in an Air Turbo Rocket-Reference-Cited by-同舟云学术

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Operation matching model and analysis between an air inlet and a compressor in an Air Turbo Rocket

Published:2018-10 Issue: Volume:81 Page:306-315
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Liu Yang^ORCID,Gao Yonggang,Pu Xiaohang,Li Jiang,He Guo-qiang

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

1. Advantage of ethanol fuel for gas generator cycle air turbo ramjet engine;Minato;Aerosp. Sci. Technol.,2016

2. ATR propulsion system design and vehicle integration;Bossard,1988

3. Conceptual study of a combined-cycle engine for an aerospace plane;Kanda;J. Propuls. Power,2012

4. An overview of advanced concepts for near space systems;Young;AIAA J.,2009

5. Development study on air turbo-ramjet for space plane;Tanatsugu;J. Gas Turbine Soc. Jpn.,2002

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