Numerical simulations of single and multi-staged injection of H2 in a supersonic scramjet combustor
- DOI
- 10.1016/j.jppr.2014.12.001
- Published
- 2014-12
- Container
- Propulsion and Power Research
- Publisher
- Elsevier BV
- Open access
- unknown
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Cite this work
BibTeX
@article{allodium:10.1016/j.jppr.2014.12.001,
title = {Numerical simulations of single and multi-staged injection of H2 in a supersonic scramjet combustor},
author = {L. Abu-Farah and O.J. Haidn and H.-P. Kau},
year = {2014},
journal = {Propulsion and Power Research},
doi = {10.1016/j.jppr.2014.12.001},
url = {https://doi.org/10.1016/j.jppr.2014.12.001}
}RIS
TY - JOUR TI - Numerical simulations of single and multi-staged injection of H2 in a supersonic scramjet combustor AU - L. Abu-Farah AU - O.J. Haidn AU - H.-P. Kau PY - 2014 JO - Propulsion and Power Research DO - 10.1016/j.jppr.2014.12.001 UR - https://doi.org/10.1016/j.jppr.2014.12.001 ER -
APA
Abu-Farah, L., Haidn, O., & Kau, H. (2014). Numerical simulations of single and multi-staged injection of H2 in a supersonic scramjet combustor. Propulsion and Power Research. https://doi.org/10.1016/j.jppr.2014.12.001
Source records
- crossref · retrieved 2026-11-09T17:45:24.202Z