All Stories

  1. NOx Emission Prediction of a Lean Premixed Hydrogen Combustor via Reactor Network Analysis
  2. Numerical Investigation on the Use of Plasma Actuators for Separation Control in Over-Expanded Nozzles
  3. Optimization of Solid Rocket Motor Grains Exploiting Non-Uniform Ballistic Properties of 3D-Printed Propellants
  4. Numerical Validation of a Swirl Injection Model for a Paraffin-Based Hybrid Rocket Engine
  5. Multi-Fidelity Modeling of a Lean Premixed Swirl-Stabilized Hydrogen Burner With Axial Air Injection
  6. Innovative Rocket Propellants: 3D Printing with Photocurable Materials
  7. Comparison of Methods for Thermodynamic Modelling of Cryogenic Storage Systems for Aerospace Applications
  8. Towards the Integration of Surrogate Models in the Robust Optimization of Hybrid Rocket Engines
  9. Modeling a Hydrogen-Powered Jet Engine for Cleaner Air Travel
  10. Design Optimization of a Mg/CO2 Hybrid Rocket Engine for Mars Ascent Vehicles
  11. A Numerical Method for Burnback Analysis of UV-cured Solid Rocket Propellant Grains
  12. Numerical Investigation of Different Configurations for Hydrogen Fuelled Jet Engine Combustors
  13. Swirl Injection Modeling for Paraffin-Based Hybrid Rocket Engines Combustion Instabilities
  14. Multiphysics modelling for a hybrid rocket engine with liquefying fuel: a sensitivity analysis on combustion instability
  15. Optimal battery selection for hybrid rocket engine
  16. Low-order models for low-frequency combustion instability in hybrid rocket engines
  17. Uncertainty Analysis and Robust Design for a Hybrid Rocket Upper Stage
  18. Robust Design of Hybrid Rocket Engine for Small Satellite Launchers