Numerical framework for transcritical real-fluid reacting flow simulations using the flamelet progress variable approach
- DOI
- 10.2514/6.2017-0143
- Published
- 2017-01-05
- Container
- 55th AIAA Aerospace Sciences Meeting
- Publisher
- American Institute of Aeronautics and Astronautics
- Open access
- unknown
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Cite this work
BibTeX
@article{allodium:10.2514/6.2017-0143,
title = {Numerical framework for transcritical real-fluid reacting flow simulations using the flamelet progress variable approach},
author = {Peter C. Ma and Daniel Banuti and Jean-Pierre Hickey and Matthias Ihme},
year = {2017},
journal = {55th AIAA Aerospace Sciences Meeting},
doi = {10.2514/6.2017-0143},
url = {https://doi.org/10.2514/6.2017-0143}
}RIS
TY - JOUR TI - Numerical framework for transcritical real-fluid reacting flow simulations using the flamelet progress variable approach AU - Peter C. Ma AU - Daniel Banuti AU - Jean-Pierre Hickey AU - Matthias Ihme PY - 2017 JO - 55th AIAA Aerospace Sciences Meeting DO - 10.2514/6.2017-0143 UR - https://doi.org/10.2514/6.2017-0143 ER -
APA
Ma, P. C., Banuti, D., Hickey, J., & Ihme, M. (2017). Numerical framework for transcritical real-fluid reacting flow simulations using the flamelet progress variable approach. 55th AIAA Aerospace Sciences Meeting. https://doi.org/10.2514/6.2017-0143
Source records
- crossref · retrieved 2026-09-27T07:26:10.988Z