<?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%">Ma, John Z.</style></author><author><style face="normal" font="default" size="100%">Bao, Weimin</style></author><author><style face="normal" font="default" size="100%">Wang, Jian-Ping</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">Experimental research of the performance and pressure gain in continuous detonation engines with aerospike nozzles</style></title><secondary-title><style face="normal" font="default" size="100%">Aerospace Science and Technology</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%">Sept</style></date></pub-dates></dates><urls><web-urls><url><style face="normal" font="default" size="100%">http://dx.doi.org/10.1016/j.ast.2023.108464</style></url></web-urls></urls><publisher><style face="normal" font="default" size="100%">Elsevier BV</style></publisher><volume><style face="normal" font="default" size="100%">140</style></volume><pages><style face="normal" font="default" size="100%">108464</style></pages><language><style face="normal" font="default" size="100%">eng</style></language></record></records></xml>