Numerical investigation of an RBCC combustor during ramjet/scramjet mode transition

Joseph Salloum, Michael Candon, Andrew Ridings, Hideaki Ogawa, Masatoshi Kodera, Shuichi Ueda

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

Rocket-based Combined-Cycle (RBCC) engines offer a promise for efficient and flexible propulsion over a large Mach number range by combining rocket and ramjet/scramjet technology. To achieve this, an RBCC engine uses four different modes of operation: rocket, ramjet, scramjet and dual-mode. During operation, the engine must make the transition from subsonic to supersonic combustion, i.e., ramjet to scramjet mode. The objective of this study is to gain physical insight into the ramjet-scramjet-ramjet mode transition by elucidating the underlying mechanics. Numerical simulations with chemical reactions have been performed for the transient flowfields of a two-dimensional RBCC combustor by using an unsteady Reynolds-Averaged Navier-Stokes solver. Mode transition is effected by changing the flow rate of the secondary hydrogen fuel injectors installed on the top and bottom walls of the combustor. A parametric study was conducted to investigate the characteristic and behavior of RBCC combustion in mode transition. The results indicated that transition is affected considerably by the presence and development of flow separation and pseudo-shock structures near fuel injectors. The complex effects of aerodynamic and aerothermal interactions on the transient flowfields and performance, along with a hysteresis observed between the scramjet-to-ramjet and ramjet-to-scramjet transition processes.

Original languageEnglish
Title of host publicationAIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
Edition210059
ISBN (Print)9781624105241
DOIs
Publication statusPublished - Jan 1 2018
Externally publishedYes
EventAIAA Aerospace Sciences Meeting, 2018 - Kissimmee, United States
Duration: Jan 8 2018Jan 12 2018

Publication series

NameAIAA Aerospace Sciences Meeting, 2018
Number210059

Other

OtherAIAA Aerospace Sciences Meeting, 2018
CountryUnited States
CityKissimmee
Period1/8/181/12/18

Fingerprint

Rockets
Combustors
Engines
Hydrogen fuels
Flow separation
Propulsion
Mach number
Hysteresis
Chemical reactions
Aerodynamics
Mechanics
Flow rate
Computer simulation

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this

Salloum, J., Candon, M., Ridings, A., Ogawa, H., Kodera, M., & Ueda, S. (2018). Numerical investigation of an RBCC combustor during ramjet/scramjet mode transition. In AIAA Aerospace Sciences Meeting (210059 ed.). (AIAA Aerospace Sciences Meeting, 2018; No. 210059). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2018-0886

Numerical investigation of an RBCC combustor during ramjet/scramjet mode transition. / Salloum, Joseph; Candon, Michael; Ridings, Andrew; Ogawa, Hideaki; Kodera, Masatoshi; Ueda, Shuichi.

AIAA Aerospace Sciences Meeting. 210059. ed. American Institute of Aeronautics and Astronautics Inc, AIAA, 2018. (AIAA Aerospace Sciences Meeting, 2018; No. 210059).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Salloum, J, Candon, M, Ridings, A, Ogawa, H, Kodera, M & Ueda, S 2018, Numerical investigation of an RBCC combustor during ramjet/scramjet mode transition. in AIAA Aerospace Sciences Meeting. 210059 edn, AIAA Aerospace Sciences Meeting, 2018, no. 210059, American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA Aerospace Sciences Meeting, 2018, Kissimmee, United States, 1/8/18. https://doi.org/10.2514/6.2018-0886
Salloum J, Candon M, Ridings A, Ogawa H, Kodera M, Ueda S. Numerical investigation of an RBCC combustor during ramjet/scramjet mode transition. In AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA. 2018. (AIAA Aerospace Sciences Meeting, 2018; 210059). https://doi.org/10.2514/6.2018-0886
Salloum, Joseph ; Candon, Michael ; Ridings, Andrew ; Ogawa, Hideaki ; Kodera, Masatoshi ; Ueda, Shuichi. / Numerical investigation of an RBCC combustor during ramjet/scramjet mode transition. AIAA Aerospace Sciences Meeting. 210059. ed. American Institute of Aeronautics and Astronautics Inc, AIAA, 2018. (AIAA Aerospace Sciences Meeting, 2018; 210059).
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