Numerical investigation of flow and combustion in a single-element GCH4/GOX rocket combustor

C. Roth; O. Haidn; A. Chemnitz; T. Sattelmayer; Y. Daimon; G. Frank; H. Müller; J. Zips; M. Pfitzner; R. Keller; P. Gerlinger; D. Maestro; B. Cuenot; H. Riedmann; L. Selle

doi:10.2514/6.2016-4995

Numerical investigation of flow and combustion in a single-element GCH₄/GOX rocket combustor

C. Roth, O. Haidn, A. Chemnitz, T. Sattelmayer, Y. Daimon, G. Frank, H. Müller, J. Zips, M. Pfitzner, R. Keller, P. Gerlinger, D. Maestro, B. Cuenot, H. Riedmann, L. Selle

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

19 Scopus citations

Abstract

The flow and combustion in a GCH₄/GOX single-element rocket combustor is analysed by several groups using different numerical models and tools. The tools and simulation setups vary with respect to modeling fidelity and computational expense. A short overview of the tools and the individual simulation setups is given. The focus of the paper is the comparison of the results obtained by the different groups as well as with experimental data. This encompasses the study of specific features of the combustor flow among the different simulations, as well as the validation with typical rocket engine design and performance parameters, such as wall heat flux and combsution pressure, gained from hot firing tests.

Original language	English
Title of host publication	52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624104060
DOIs	https://doi.org/10.2514/6.2016-4995
State	Published - 2016
Event	52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016 - Salt Lake City, United States Duration: 25 Jul 2016 → 27 Jul 2016

Publication series

Name	52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016

Conference

Conference	52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
Country/Territory	United States
City	Salt Lake City
Period	25/07/16 → 27/07/16

Access to Document

10.2514/6.2016-4995

Cite this

Roth, C., Haidn, O., Chemnitz, A., Sattelmayer, T., Daimon, Y., Frank, G., Müller, H., Zips, J., Pfitzner, M., Keller, R., Gerlinger, P., Maestro, D., Cuenot, B., Riedmann, H., & Selle, L. (2016). Numerical investigation of flow and combustion in a single-element GCH₄/GOX rocket combustor. In 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016 (52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2016-4995

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title = "Numerical investigation of flow and combustion in a single-element GCH4/GOX rocket combustor",

abstract = "The flow and combustion in a GCH4/GOX single-element rocket combustor is analysed by several groups using different numerical models and tools. The tools and simulation setups vary with respect to modeling fidelity and computational expense. A short overview of the tools and the individual simulation setups is given. The focus of the paper is the comparison of the results obtained by the different groups as well as with experimental data. This encompasses the study of specific features of the combustor flow among the different simulations, as well as the validation with typical rocket engine design and performance parameters, such as wall heat flux and combsution pressure, gained from hot firing tests.",

author = "C. Roth and O. Haidn and A. Chemnitz and T. Sattelmayer and Y. Daimon and G. Frank and H. M{\"u}ller and J. Zips and M. Pfitzner and R. Keller and P. Gerlinger and D. Maestro and B. Cuenot and H. Riedmann and L. Selle",

note = "Publisher Copyright: {\textcopyright} 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016 ; Conference date: 25-07-2016 Through 27-07-2016",

year = "2016",

doi = "10.2514/6.2016-4995",

language = "English",

isbn = "9781624104060",

series = "52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

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Roth, C, Haidn, O, Chemnitz, A, Sattelmayer, T, Daimon, Y, Frank, G, Müller, H, Zips, J, Pfitzner, M, Keller, R, Gerlinger, P, Maestro, D, Cuenot, B, Riedmann, H & Selle, L 2016, Numerical investigation of flow and combustion in a single-element GCH₄/GOX rocket combustor. in 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, American Institute of Aeronautics and Astronautics Inc, AIAA, 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, United States, 25/07/16. https://doi.org/10.2514/6.2016-4995

Numerical investigation of flow and combustion in a single-element GCH₄/GOX rocket combustor. / Roth, C.; Haidn, O.; Chemnitz, A. et al.
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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