机译:基于自适应网格细化的超音速可燃混合物爆轰起爆的数值模拟
Science and Technology on Scramjet Laboratory, National Univ. of Defense Technology, Hunan, Changsha 410073, China;
Science and Technology on Scramjet Laboratory, National Univ. of Defense Technology, Hunan, Changsha 410073, China;
Science and Technology on Scramjet Laboratory, National Univ. of Defense Technology, Hunan, Changsha 410073, China;
Computational Fluid Dynamics, German Aerospace Center (DLR), Institute of Aerodynamics and Flow Technology, Bunsenstrasse 10, 37073 Goettingen, Germany;
Science and Technology on Scramjet Laboratory, National Univ. of Defense Technology, Hunan, Changsha 410073, China;
Science and Technology on Scramjet Laboratory, National Univ. of Defense Technology, Hunan, Changsha 410073, China;
Adaptive mesh refinement; Supersonic combustible mixtures; Hot jet; Detonation initiation; Pisiform detonation cell;
机译:基于自适应网格细化的超声速可燃混合物三维爆轰燃烧模拟及详细反应模型
机译:热喷对超声速可燃混合物中爆炸起爆和传播的影响
机译:超声速可燃混合物中脉冲热流爆轰控制的数值研究
机译:具有不均匀物质的超音速可燃混合物起爆和传播的数值模拟
机译:热分层反应混合物中的热点表征和爆轰起始=热分层反应混合物中的热点表征和引发的引发
机译:H2–O2混合物爆炸和爆轰数值模拟的两步动力学模型
机译:基于自适应网格细化的超音速可燃混合物中三维爆轰燃烧模拟及详细反应模型
机译:自适应重叠网格上CsCm(保守上特征法)超音速射流排气流的精确数值模拟