<?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%">Zhang, Yunzhen</style></author><author><style face="normal" font="default" size="100%">Ma, John Z.</style></author><author><style face="normal" font="default" size="100%">Kevin Wu</style></author><author><style face="normal" font="default" size="100%">Cheng, Miao</style></author><author><style face="normal" font="default" size="100%">Sheng, Zhaohua</style></author><author><style face="normal" font="default" size="100%">Rong, Guangyao</style></author><author><style face="normal" font="default" size="100%">Shen, Dawen</style></author><author><style face="normal" font="default" size="100%">Jianping Wang</style></author><author><style face="normal" font="default" size="100%">Shujie Zhang</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">Analysis on Propulsive Performance of Hollow Rotating Detonation Engine with Laval Nozzle</style></title><secondary-title><style face="normal" font="default" size="100%">Journal of Propulsion and Power</style></secondary-title></titles><dates><year><style  face="normal" font="default" size="100%">2023</style></year><pub-dates><date><style  face="normal" font="default" size="100%">jun</style></date></pub-dates></dates><urls><web-urls><url><style face="normal" font="default" size="100%">https://doi.org/10.2514%2F1.b38830</style></url></web-urls></urls><publisher><style face="normal" font="default" size="100%">American Institute of Aeronautics and Astronautics (AIAA)</style></publisher><pages><style face="normal" font="default" size="100%">1–15</style></pages><language><style face="normal" font="default" size="100%">eng</style></language></record></records></xml>