All Stories

  1. Advances and challenges in developing a stochastic model for multi-scale fluid dynamic simulation: One-dimensional turbulence
  2. One-dimensional turbulence modeling of compressible flows. I. Conservative Eulerian formulation and application to supersonic channel flow
  3. One-dimensional turbulence modeling of compressible flows: II. Full compressible modification and application to shock–turbulence interaction
  4. A consistent scheme of the high-speed source term in probability density function methods for supersonic flows
  5. A numerical study of the rapid deflagration-to-detonation transition
  6. Flame–turbulence interactions during flame acceleration using solid and fluid obstacles
  7. Conservative compressible one-dimensional turbulence formulation and application to high-Reynolds-number compressible turbulent channel flows
  8. Generation mechanism of a new type of unburnt gas pocket and its influences on the detonation-wave/boundary-layer interaction
  9. Detonation Stabilization in Supersonic Flow: Effects of Suction Boundaries
  10. Separation induced low-frequency unsteadiness in a supersonic combustor with single-side expansion
  11. Detonation Interaction with Cavity in Supersonic Combustible Mixture
  12. Diffusion and mixing effects in hot jet initiation and propagation of hydrogen detonations
  13. Experimental investigation of combustion stabilization modes in a cavity-based supersonic combustor with different wall divergence angles
  14. Continuous 100 Hz planar laser-induced fluorescence applied to the study of combustion processes
  15. Analysis of Separation Modes Variation in a Scramjet Combustor with Single-Side Expansion
  16. Dynamic combustion characteristics in a rectangular supersonic combustor with single-side expansion
  17. Detonation Simulations in Supersonic Combustible Mixtures with Nonuniform Species
  18. Coupled Heat Transfer of Supercritical n-Decane in a Curved Cooling Channel
  19. Flow Mechanism in a Hypersonic Sidewall Compression Inlet with a Rectangular-to-Circular Isolator
  20. Flight Acceleration Effect on Heat Transfer Deterioration of Actively Cooled Scramjet Engines
  21. Research on the effect of cowl lip angle on the accelerating start process of a two-dimensional hypersonic inlet
  22. Numerical simulation on detonation initiation and propagation in supersonic combustible mixtures with nonuniform species
  23. Laser-Induced Plasma Ignition of Hydrocarbon Fuel in Supersonic Flows
  24. Numerical study of coupled heat transfer of supercritical n-decane in a curved cooling channel
  25. Efficient Thermodynamic Properties Reconstruction Method with Adaptive Triangular Mesh
  26. Detonation Initiation and Propagation in Nonuniform Supersonic Combustible Mixtures
  27. Investigation on Hypersonic Inlet Starting Process in Continuous Freejet Wind Tunnel
  28. Simulation of heat transfer of mildly-cracked n-decane in a tube with 3-dimensional equation of state look-up table
  29. Numerical analysis of heat transfer deterioration of China RP-3 aviation kerosene in a circular tube at supercritical pressures