All Stories

  1. Innovative Design of Waste Heat Recovery Heat Exchangers
  2. Coupled unsteady RANS and FW-H methodology for aeroacoustics prediction of high-speed propellers
  3. A novel design-point computational program for thermal power plants applications: energy, exergy and economic (3E) analysis
  4. A parametric study of squealer tip geometries applied in a hydraulic axial turbine used in a rocket engine turbopump
  5. Evaluation of an effective and robust implicit time-integration numerical scheme for Navier-Stokes equations in a CFD solver for compressible flows
  6. Effect of tip clearance on cavitating flow of a hydraulic axial turbine applied in turbopump
  7. Preconditioning methods for compressible flow CFD codes: Revisited
  8. Comparative Study Between Structured and Unstructured Meshes Applied in Turbopump’s Hydraulic Turbine
  9. Evaluation of a Machine Learning Turbulence Model in a Square Transverse Jet in Crossflow
  10. Interactive Learning Platform for Turbine Design Using Reduced Order Methods
  11. A Proposal for Passive Wall Treatment Applied in High Performance Axial Flow Compressors
  12. Thermoeconomic comparison between the organic flash cycle and the novel organic Rankine flash cycle (ORFC)
  13. Thermoeconomic optimization of organic Rankine bottoming cycles for micro gas turbines
  14. Air conditioning systems for aeronautical applications: a review
  15. Preliminary Design of Axial Flow Turbine for a Small Jet Engine
  16. Implementing a Preconditioning Technique in A RANS Compressible Code to Accelerate the Convergence Rate for Low-Speed Flows
  17. Applying a Preconditioning Technique to the Euler Equations to Accelerate the Convergence Rate for Low-Speed Flows
  18. Helicopter Air Data Systems Calibration Using DGPS
  19. A Review on Combining Micro Gas Turbines with Organic Rankine Cycles
  20. Exergy-based parallel between steam- and combined-cycle power plant configurations burning blast furnace gas
  21. Influence of Variable Geometry Compressor on Transient Performance of Counter-Rotating Open Rotor Engines
  22. Optimal wingtip device design for transport airplane
  23. Development and convergence analysis of an effective and robust implicit Euler solver for 3D unstructured grids
  24. Numerical Investigation of Film and Impingement Cooling Schemes for Gas Turbine Application
  25. Turbopump Booster Turbine Performance: Comparison Between Monophase and Multiphase Flows Using CFD
  26. A Propeller Model for Steady-State and Transient Performance Prediction of Turboprop and Counter-Rotating Open Rotor Engines
  27. Run time Assessment for Gas Turbine Performance Simulation
  28. Simulation of a centrifugal compressor to obtain the characteristic map through computational effort
  29. In-flight thrust determination for high-bypass-ratio turbofan using residual error methodology
  30. An evaluation of the tip clearance effects on turbine efficiency for space propulsion applications considering liquid rocket engine using turbopumps
  31. Real-Time Gas Turbine Model for Performance Simulations
  32. Parallel Between Rankine and Combined-Cycle Power Plants Configurations Burning Blast Furnace Gas
  33. Performance Evaluation of a Hydraulic Turbine Used As a Turbodrill for Oil and Gas Applications in Post-Salt Environment
  34. Project-Based Learning Applied in Turbopump Discipline at ITA Using 1D and 3D Numerical Simulations of a Booster Turbine Installed in the Space Shuttle Main Engine
  35. Numerical investigation of a HPT with different rotor tip configurations in terms of pressure ratio and efficiency
  36. Combined Cycle Performance Evaluation and Dynamic Response Simulation
  37. Characterization of an ethanol fueled heavy-duty engine powering a generator set
  38. Implicit
  39. Study and Analysis of a Power Turbine Preliminary Design for a Small Turboshaft
  40. One Stage Power Turbine Preliminary Design and Analysis
  41. Gas Turbine Course’s Teaching Process at Instituto Tecnológico de Aeronáutica: Theory and Laboratory
  42. Experiences on Project-Based-Classes for Turbomachine Design in an Aerospace Engineering Undergraduate Program
  43. Evaluation of Different Squealer Cavity Configurations in a HPT Blade Tip Region and its Influence on the Heat Transfer
  44. A Step Further on the Control of Acceleration of Gas Turbines With Controlled Variable Geometry and Combustion Emissions
  45. Technical evaluation of vehicle ignition systems: conduct differences between a high energy capacitive system and a standard inductive system
  46. A Study of the Heat Transfer in Winglet and Squealer Rotor Tip Configurations for a Non-Cooled HPT Blade Based on CFD Calculations
  47. The Flow Machines Course at the Technological Institute of Aeronautics for Mechanical-Aeronautical Engineering Undergraduate Course
  48. Gas Turbine Transients With Controlled Variable Geometry
  49. Performance Evaluation of a 5 kN Gas Turbine Based on Specially Designed Components
  50. Numerical Tools for High Performance Axial Compressor Design for Teaching Purpose
  51. Comparison Between Unstructured and Structured Meshes With Different Turbulence Models for a High Pressure Turbine Application
  52. An Axial Flow Compressor for Operation With Humid Air and Water Injection
  53. Influence of Variable Geometry Transients on the Gas Turbine Performance
  54. Performance Study of a 1 MW Gas Turbine Using Variable Geometry Compressor and Turbine Blade Cooling
  55. An Axial-Flow Compressor for Operation With Humid Air and Water Injection
  56. An Object-Oriented Parallel Finite-Volume CFD Code
  57. Nacelle Design for Mixed Turbofan Engines
  58. Gas Turbine Performance Simulation Using an Optimized Axial Flow Compressor