Influence of injection angles on flow structures and mixing properties in a supersonic combustor at low Mach supersonic crossflow. [PDF]
Zhang L+4 more
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Controlling hypersonic boundary layer transition with localized cooling and metasurface treatments. [PDF]
Oz F, Kara K.
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A Novel Hypersonic Target Trajectory Estimation Method Based on Long Short-Term Memory and a Multi-Head Attention Mechanism. [PDF]
Xu Y, Pan Q, Wang Z, Hu B.
europepmc +1 more source
A New Facility Will Harness Plasma to Guide Interplanetary Craft. [PDF]
Bourzac K.
europepmc +1 more source
Gas Kinetic Scheme Coupled with High-Speed Modifications for Hypersonic Transition Flow Simulations. [PDF]
Li C+5 more
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Nonlinear Modeling Study of Aerodynamic Characteristics of an X38-like Vehicle at Strong Viscous Interaction Regions. [PDF]
Jiang D, Wang P, Li J, Mao M.
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Thermal modal analysis of hypersonic composite wing on transient aerodynamic heating. [PDF]
Wang K+5 more
europepmc +1 more source
Development of combined hypersonic test facility for aerothermodynamic testing. [PDF]
Yang S, Choi I, Park G.
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Effect of Kerosene Dual-Jet Spacing on the Mixing and Combustion Characteristics of a Scramjet Combustor. [PDF]
Peng SS+5 more
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