Climbing performance analysis of rocket-based combined cycle engine powered aircraft-Reference-Cited by-同舟云学术

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Climbing performance analysis of rocket-based combined cycle engine powered aircraft

Published:2019-09 Issue: Volume:162 Page:135-144
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Jia Yicong,Ye Wei,Cui Peng,Xu Wanwu

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. US national center for hypersonic combined cycle propulsion: an overview;McDaniel,2009

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

3. Ascent trajectory design method for RBCC-powered vehicle [J];Xiang;Acta Aeronautica Astronautica Sinica,2010

4. Ascent phase trajectory optimization for vehicle with multi-combined cycle engine based on improved particle swarm optimization;Zhou;Acta Astronaut.,2017

5. Optimization of the rocket mode trajectory in a rocket based combined cycle (RBCC) engine powered SSTO vehicle;FOSTER,1989

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2. Numerical Investigation on the Effect of Fuel-Rich Degree in the RBCC Engine under the Ejector Mode;International Journal of Aerospace Engineering;2024-02-06

3. Effects of excess oxidizer coefficient on RBCC engine performance in ejector mode: A theoretical investigation;Energy;2024-02

4. Experimental and numerical study on RBCC engines performance in simultaneous and combustion cycle;International Communications in Heat and Mass Transfer;2024-01

5. Experimental study of rocket plume expansion in the rocket-based combined-cycle engine under the ejector mode;Aerospace Science and Technology;2023-07

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