All Stories

  1. Optimization of Solid Rocket Motor Grains Exploiting Non-Uniform Ballistic Properties of 3D-Printed Propellants
  2. Numerical Validation of a Swirl Injection Model for a Paraffin-Based Hybrid Rocket Engine
  3. Multi-Fidelity Modeling of a Lean Premixed Swirl-Stabilized Hydrogen Burner With Axial Air Injection
  4. Innovative Rocket Propellants: 3D Printing with Photocurable Materials
  5. Comparison of Methods for Thermodynamic Modelling of Cryogenic Storage Systems for Aerospace Applications
  6. Modeling a Hydrogen-Powered Jet Engine for Cleaner Air Travel
  7. Can Reusable Heavy-lift Rockets perform Vertical Landing with an Aerospike Engine?
  8. Design Optimization of a Mg/CO2 Hybrid Rocket Engine for Mars Ascent Vehicles
  9. A Numerical Method for Burnback Analysis of UV-cured Solid Rocket Propellant Grains
  10. Numerical Investigation of Different Configurations for Hydrogen Fuelled Jet Engine Combustors
  11. Swirl Injection Modeling for Paraffin-Based Hybrid Rocket Engines Combustion Instabilities
  12. Multiphysics modelling for a hybrid rocket engine with liquefying fuel: a sensitivity analysis on combustion instability
  13. Fluidic Control of Transition in a Dual-bell Nozzle
  14. Low-order models for low-frequency combustion instability in hybrid rocket engines
  15. Preliminary study of a resonant igniter for rocket engines
  16. Acoustic Excitation as Triggering Mechanism of the “DC Shift” in Hybrid Rockets
  17. Uncertainty Analysis and Robust Design for a Hybrid Rocket Upper Stage
  18. Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction
  19. Robust Design of Hybrid Rocket Engine for Small Satellite Launchers
  20. Plasma Actuator–Assisted Rocket Nozzle for Improved Launcher Performance
  21. Optimization of Active Debris Removal Missions with Multiple Targets
  22. Novel Comprehensive Technique for Hybrid Rocket Experimental Ballistic Data Reconstruction
  23. Pressure-Measurement Based Estimation of Fuel Regression Rate in Hybrid Rockets
  24. Modeling of Saturated and Superheated N2O Heat Transfer Rates, with Experimental Verification
  25. A Straightfotward Approach for Robust Design of Hybrid Rocket Engine Upper Stage
  26. Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage
  27. Analysis of Acoustics and Vortex Shedding Interactions in Hybrid Rocket Motors
  28. Optimization of Hybrid Upper-Stage Motor with Coupled Evolutionary/Indirect Procedure
  29. Optimization of an Advanced Open Rotor Engine for Civil Transport
  30. Optimization of Hybrid Propellant Mars Ascent Vehicle
  31. Efficient Missions to Potentially Hazardous Object 2013 TV135