@inproceedings{9f786432db89447c9f02a1639710eafd,
title = "Comparison of a single and multi-injector GOX-GCH4 combustion chamber",
abstract = "The present study aims to contribute to the understanding of the thermal transfer and mixing processes for GCH4/GOX single and multi-element shear coaxial injector. The experimental data provide a benchmark for the validation of CFD numerical tools for the new propellant combination and offer an example of scaling methodology for multi-element and single-element chambers. A high-pressure facility operated at conditions typical of rocket engines is used. Experimental investigations as well as numerical simulations provide detailed information about the heat flux at the hot inner walls of the combustion chamber and a flame structure for pressures up to 20 bar. Heat flux was calculated by solving 3D unsteady heat conduction equation using the inverse method.",
author = "Celano, {M. P.} and S. Silvestri and C. Bauer and N. Perakis and G. Schlieben and Haidn, {O. J.}",
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",
language = "English",
isbn = "9781624104060",
series = "52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016",
}