All Stories

  1. Experimental and theoretical assessment of carbon capture onto activated carbon at subcritical and supercritical conditions
  2. Techno-economic feasibility of CO2 utilization in sustainable energy harvesting: Energy–Exergy–Economic–Environmental (4E) analysis
  3. Assessment of Ecofriendly Zeotropic Working Fluids in Organic Rankine Cycle for Renewable Energy Harvesting
  4. Microscopic spray measurements of non-reacting alternative jet fuel: Effect of ambient gas temperature
  5. Global opportunities and challenges on net-zero CO2 emissions towards a sustainable future
  6. Computational study of the effect of cavity geometry on the supersonic mixing and combustion of ethylene
  7. Effects of nanoscale fuel additives on properties and non-reacting spray performance of alternative, conventional and blended jet fuels at elevated ambient conditions
  8. Numerical investigation of the local and global supersonic combustion characteristics of ethylene fuel
  9. Performance Maximization by Temperature Glide Matching in Energy Exchangers of Cooling Systems Operating with Natural Hydrocarbon/CO2 Refrigerants
  10. Macroscopic spray performance of alternative and conventional jet fuels at non-reacting, elevated ambient conditions
  11. Thermodynamic Study on Blends of Hydrocarbons and Carbon Dioxide as Zeotropic Refrigerants
  12. Nanomaterials for detection and removal of gases
  13. Spray Characteristics of Alternative Jet Fuel at Elevated Ambient Conditions
  14. Effect of Carbon Dioxide on the Laminar Burning Speed of Propane–Air Mixtures
  15. Application of Nanoparticles in Clean Fuels
  16. Spray Performance of Alternative Jet Fuel Based Nanofuels at High-Ambient Conditions
  17. Comparison of Near-Nozzle Spray Performance of Gas-to-Liquid and Jet A-1 Fuels Using Shadowgraph and Phase Doppler Anemometry
  18. The effects of alumina nanoparticles as fuel additives on the spray characteristics of gas-to-liquid jet fuels
  19. Theoretical Prediction of Laminar Burning Speed and Ignition Delay of Gas to Liquid Fuel
  20. Effect of Nanoparticles on the Fuel Properties and Spray Performance of Aviation Turbine Fuel
  21. Theoretical Prediction of Laminar Burning Speed and Ignition Delay Time of Gas-to-Liquid Fuel
  22. Influence of Nanoparticles on Spray Performance of Alternative Jet Fuels
  23. Experimental investigation of spray characteristics of alternative aviation fuels
  24. Experimental Study of the Effect of Fuel Properties on Spray Performance of Alternative Jet Fuel
  25. EFFECT OF FUEL PROPERTIES ON SPRAY CHARACTERISTICS OF ALTERNATIVE JET FUELS USING GLOBAL SIZING VELOCIMETRY
  26. Spray Characteristics of Fischer-Tropsch Alternate Jet Fuels
  27. Numerical Simulation of Particle-Laden Coaxial Turbulent Jets
  28. Numerical simulation of coaxial turbulent jet with and without discrete particles
  29. Surrogate Model Design for GtL Kerosene
  30. Spray characterization of gas-to-liquid alternative aviation fuels
  31. Effect of GTL-Like Jet Fuel Composition on GT Engine Altitude Ignition Performance: Part I—Combustor Operability
  32. Investigation of GTL-Like Jet Fuel Composition on GT Engine Altitude Ignition and Combustion Performance: Part II—Detailed Diagnostics
  33. Numerical simulation of particle-laden coaxial turbulent jets
  34. Effects of GTL fuels on aircraft gas turbine altitude ignition combustor operability
  35. GTL fuels and their effects on aircraft aas turbine altitude ignition – detailed diagnostics
  36. Numerical Investigation of the Supersonic Combustion of Kerosene in a Strut-Based Combustor
  37. Mixing and Combustion Characteristics of Kerosene in a Model Supersonic Combustor
  38. Investigation of the effect of chemistry models on the numerical predictions of the supersonic combustion of hydrogen
  39. A Comparison of Numerical Predictions of Supersonic Combustion of Hydrogen Using Different Chemistry Models in a Model Combustor
  40. A comparison of the numerical predictions of the supersonic combustion of Hydrogen using the S-A and SST k – ω models
  41. Effect of swirl on lean flame limits of pilot-stabilized open premixed turbulent flames