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机译:双燃烧冲压发动机流场和性能的实验和数值研究
Science and Technology on Scramjet Laboratory, National University of Defense Technology, ChangSha 410073, PR China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, ChangSha, PR China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, ChangSha, PR China;
Dual combustion ramjet; direct-connected experiment; numerical simulation; performance; flow fields;
机译:旋流式固体燃料冲压发动机着火和燃烧稳定性的实验和数值研究
机译:Freejet双燃烧冲压发动机性能的实验研究
机译:旋流对固体燃料冲压发动机燃烧特性和性能影响的实验研究
机译:Onera-LAERTE设施的LAPCAT-Ⅱ双模Ramjet燃烧室中热气流中氢的燃烧-实验和数值研究
机译:高超声速冲击诱导的冲压燃料流场的数值模拟。
机译:雪弗龙混合器内部空气动力和燃烧性能的数值研究
机译:涡流对固体燃料冲压发动机燃烧特性影响的实验研究