Survey on key techniques of rocket-based combined-cycle engine in ejector mode

Z Dong, M Sun, Z Wang, J Chen, Z Cai - Acta Astronautica, 2019 - Elsevier
A rocket-based combined-cycle (RBCC) engine synthetically integrates a traditional rocket
engine with an airbreathing engine, effectively combining both advantages of high thrust-to …

Performance validation approach for the GTX air-breathing launch vehicle

CJ Trefny, JM Roche - Combustion, Airbreathing Propulsion …, 2002 - ntrs.nasa.gov
The primary objective of the GTX effort is to determine whether or not air-breathing
propulsion can enable a launch vehicle to achieve orbit in a single stage. Structural weight …

Direct-connect ejector ramjet combustor experiment

H Kamhawi, T Krivanek, S Thomas… - 41st Aerospace Sciences …, 2003 - arc.aiaa.org
Results of the first phase of hydrogen-fueled rocket-based combined-cycle (RBCC) flow path
testing are presented. The focus of this study was to evaluate a semi-axisymmetric, single …

RBCC 引射/亚燃模态过渡工作过程数值模拟

刘洋, 何国强, 刘佩进, 秦飞 - 推进技术, 2009 - jpt.tjjsjpt.com
针对模态过渡过程中的瞬变特性, 开展了引射/亚燃模态过渡工作过程中的RBCC
进气道/燃烧室一体化数值模拟, 计算比较了四种不同的模态过渡方案, 分析了模态过渡工作过程 …

Fuel injector design optimization for an annular SCRAMJet geometry

C Steffen - 41st Aerospace Sciences Meeting and Exhibit, 2003 - arc.aiaa.org
ABSTRACT Afour-parameter, three-level, centralcompositeexperimentdesignhasbee… the
configuration of an annular scramjet injector geometry using computational fluid dynamics …

[图书][B] Reynolds-averaged Navier-Stokes analysis of the flow through a model rocket-based combined-cycle engine with an independently-fueled ramjet stream

RB Bond - 2003 - search.proquest.com
A new concept for the low speed propulsion mode in rocket based combined cycle (RBCC)
engines has been developed as part of the NASA GTX program. This concept, called the …

[PDF][PDF] Simulation of a rocket base combined cycle exchange inlet at subsonic conditions

TSC Yuen - 2012 - repository.library.carleton.ca
Abstract Rocket Based Combined Cycle (RBCC) engines combine the high specific
impulses of air breathing engines and the large operation envelop of rockets. Such engines …

[PDF][PDF] Modelo matemático de câmaras de combustão bipropelentes

CA Valverde-Salvador - 2004 - bibdigital.sid.inpe.br
Desenvolveu-se um modelo matemático unidimensional de uma câmara de combustão de
foguete utilizando propelentes líquidos. O processo de combustão é controlado pela …

Scramjet fuel injection array optimization utilizing mixed variable pattern search with kriging surrogates

B Sparkman - 2008 - scholar.afit.edu
Fuel-air mixing analysis of scramjet aircraft is often performed through ex-perimental
research or Computational Fluid Dynamics (cfd) algorithms. Design optimization with these …

[引用][C] Research Progress in Aerospace Vehicles Propelled by Rocket-Based Combined Cycle Engines

Z Duo, QIN Fei, WEI Xianggeng… - 中国航天(英文版), 2016 - zghtywbjournal.com
Research Progress in Aerospace Vehicles Propelled by Rocket-Based Combined Cycle
Engines Page 1 RESEARCH www.aerospacechina.org AEROSPACE CHINA 21 Reviews …