All Stories

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