All Stories

  1. MHz Rate In-Situ Direct Surface Heat-Flux Measurements in a Rotating-Detonation Engine
  2. Non-Reacting VOF CFD Methodology for Single Liquid RDRE Injector
  3. Validated Reduced Methods for Realistic RDC Injection Modeling Without Chemistry
  4. Comprehensive Numerical Procedure of the THOR Non-Premixed Hydrogen-Air RDE
  5. Characterization of RDC Interaction With a Core Flow
  6. Characterization of Bladeless Power Extraction From a Rotating Detonation Rocket Combustor
  7. Shock Separation Features in Canonical Wavy Surfaces
  8. Demonstration of Frequency-Scanning Burst-Mode Filtered Rayleigh Scattering for Multi-Parameter Gas-Phase Measurements
  9. Development and characterization of high Mach nozzle using high-frequency optical and surface techniques
  10. Design, Analysis, and Test of a Cooled Rotating Detonation Combustor through axially injected stepped cooling slots
  11. Modeling of liquid injection in rotating detonation combustors
  12. Optically accessible GOx/RP-2 RDRE with MHz-rate visualization of the dynamic wave phenomena
  13. Multi-Objective Optimization and Validation of a Diodic Profile
  14. Numerical analysis on the effect of CTAP measurements in pulse and rotating detonation combustors
  15. Turbine-integrated High-pressure Optical RDE (THOR) for injection and detonation dynamics assessment
  16. AIAA aPropulsion Aerodynamic Workshop comparing various CFD codes to test data
  17. Characterization of an integrated nozzle and supersonic axial turbine with a rotating detonation combustor
  18. Aerodynamic Design and Analysis of the Hyperloop
  19. Evaluation of the unsteadiness across nozzles downstream of rotating detonation combustors
  20. Unsteady Performance of Rotating Detonation Engines with Different Exhaust Nozzles
  21. One-Dimensional Analysis of the Magnetohydrodynamic Effect in Rotating Detonation Combustors
  22. Aerodynamic Design and Analysis of the Hyperloop Pod
  23. Assessment of the Boundary Layer within a Rotating Detonation Combustor
  24. Mono-dimensional analysis of the MagnetoHydrodynamic effect in Rotating Detonation Combustors