<?xml version="1.0" encoding="UTF-8"?><xml><records><record><source-app name="Biblio" version="7.x">Drupal-Biblio</source-app><ref-type>17</ref-type><contributors><authors><author><style face="normal" font="default" size="100%">Shu-jie Zhang</style></author><author><style face="normal" font="default" size="100%">Ma, John Z.</style></author><author><style face="normal" font="default" size="100%">Jianping Wang</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">Theoretical and Numerical Investigation on Total Pressure Gain in Rotating Detonation Engine</style></title><secondary-title><style face="normal" font="default" size="100%">AIAA Journal</style></secondary-title></titles><dates><year><style  face="normal" font="default" size="100%">2020</style></year><pub-dates><date><style  face="normal" font="default" size="100%">nov</style></date></pub-dates></dates><urls><web-urls><url><style face="normal" font="default" size="100%">https://doi.org/10.2514%2F1.j059259</style></url></web-urls></urls><number><style face="normal" font="default" size="100%">11</style></number><publisher><style face="normal" font="default" size="100%">American Institute of Aeronautics and Astronautics (AIAA)</style></publisher><volume><style face="normal" font="default" size="100%">58</style></volume><pages><style face="normal" font="default" size="100%">4866–4877</style></pages><language><style face="normal" font="default" size="100%">eng</style></language></record></records></xml>