All Stories

  1. High-Pressure Turbine Aerodynamic Enhancement Using Rotor Tip Desensitization Technique
  2. Performance Analysis of Hybrid-Electric Propulsion Systems for Regional Commuter Aircraft
  3. A review of hydrogen aircraft propulsion systems: recent advances and environmental perspectives
  4. Performance and Stall Margin Evaluation of Axial Slot Casing Treatment in a Transonic Multistage Compressor
  5. Performance and Stall Margin Evaluation of Axial Slot Casing Treatment in a Transonic Multistage Compressor
  6. Winglet Geometries Applied to Rotor Blades of a Hydraulic Axial Turbine Used as a Turbopump: A Parametric Analysis
  7. Winglet Geometries Applied in Rotor Blades of a Hydraulic Axial Turbine Used as Turbopump: A Parametric Analysis
  8. Performance and optimization evaluation for integration of sCO2 power system into the aircraft propulsion system
  9. An Evaluation of Passive Wall Treatment with Circumferential Grooves at the Casing of the First and Second Blade Rotor Rows of a High-Performance Multi-Stage Axial Compressor
  10. Air Cycle Machine Modeling Applied to Aeronautical Air Conditioning Unit
  11. Gas Turbine Design Point Definition Using Economics, Environmental and Optimization Aspects
  12. Innovative Design of Waste Heat Recovery Heat Exchangers
  13. Gas Turbine Modelling and Control System Development for Offshore Applications
  14. Potential Use of Additively Manufactured Swirlers for Gas Turbine Applications
  15. An Evaluation of Passive Wall Treatment With Circumferential Grooves at the Casing of the First and Second Blade Rotor Rows of a High-performance Multi-stage Axial Compressor
  16. Liquid Rocket Engine Inducer Pump Design and Performance Evaluation
  17. Usage of an Interactive Learning Platform in Project-Based Graduate Courses for the Preliminary Design of Axial Turbines
  18. Improvement of cache utilization in a parallel CFD code through mesh reordering by Hilbert curves
  19. Modeling an Evaporative Cooling System to Improve Gas Turbines Performance
  20. Correction: Techno-economic Evaluation of the sCO2 Waste Heat Recovery System for Aircraft Engines
  21. Techno-economic Evaluation of the sCO2 Waste Heat Recovery System for Aircraft Engines
  22. Aerodynamic Analysis of Conventional and Boundary Layer Ingesting Propellers
  23. Helicopter engine simulation using flight test data
  24. Efeitos do ato de desregulamentação de 1978 na indústria aeronáutica medidos pelo método da entropia estatística
  25. Coupled unsteady RANS and FW-H methodology for aeroacoustics prediction of high-speed propellers
  26. An Evaluation of Passive Wall Treatment With Circumferential Grooves in a High-Performance Multi-Stage Axial Compressor
  27. Interactive Learning Platform for the Preliminary Design of Axial Turbines and Its Use for Graduate Courses
  28. Three-dimensional flow investigation of a high-pressure turbine with rotor tip desensitization based on Winglet geometry
  29. A novel design-point computational program for thermal power plants applications: energy, exergy and economic (3E) analysis
  30. A parametric study of squealer tip geometries applied in a hydraulic axial turbine used in a rocket engine turbopump
  31. sCO2 Waste Heat Recovery System in Aircraft Engine
  32. Evaluation of an effective and robust implicit time-integration numerical scheme for Navier-Stokes equations in a CFD solver for compressible flows
  33. Effect of tip clearance on cavitating flow of a hydraulic axial turbine applied in turbopump
  34. Evaluation of Different Turbulence Models Applied in Turbopump’s Hydraulic Turbine
  35. Preconditioning methods for compressible flow CFD codes: Revisited
  36. Comparative Study Between Structured and Unstructured Meshes Applied in Turbopump’s Hydraulic Turbine
  37. Evaluation of a Machine Learning Turbulence Model in a Square Transverse Jet in Crossflow
  38. Interactive Learning Platform for Turbine Design Using Reduced Order Methods
  39. A Proposal for Passive Wall Treatment Applied in High Performance Axial Flow Compressors
  40. Thermoeconomic comparison between the organic flash cycle and the novel organic Rankine flash cycle (ORFC)
  41. Thermoeconomic optimization of organic Rankine bottoming cycles for micro gas turbines
  42. Air conditioning systems for aeronautical applications: a review
  43. Preliminary Design of Axial Flow Turbine for a Small Jet Engine
  44. Implementing a Preconditioning Technique in A RANS Compressible Code to Accelerate the Convergence Rate for Low-Speed Flows
  45. Applying a Preconditioning Technique to the Euler Equations to Accelerate the Convergence Rate for Low-Speed Flows
  46. Helicopter Air Data Systems Calibration Using DGPS
  47. A Review on Combining Micro Gas Turbines with Organic Rankine Cycles
  48. Exergy-based parallel between steam- and combined-cycle power plant configurations burning blast furnace gas
  49. Influence of Variable Geometry Compressor on Transient Performance of Counter-Rotating Open Rotor Engines
  50. Optimal wingtip device design for transport airplane
  51. Development and convergence analysis of an effective and robust implicit Euler solver for 3D unstructured grids
  52. Numerical Investigation of Film and Impingement Cooling Schemes for Gas Turbine Application
  53. Turbopump Booster Turbine Performance: Comparison Between Monophase and Multiphase Flows Using CFD
  54. A Propeller Model for Steady-State and Transient Performance Prediction of Turboprop and Counter-Rotating Open Rotor Engines
  55. Run time Assessment for Gas Turbine Performance Simulation
  56. Simulation of a centrifugal compressor to obtain the characteristic map through computational effort
  57. In-flight thrust determination for high-bypass-ratio turbofan using residual error methodology
  58. An evaluation of the tip clearance effects on turbine efficiency for space propulsion applications considering liquid rocket engine using turbopumps
  59. Real-Time Gas Turbine Model for Performance Simulations
  60. Parallel Between Rankine and Combined-Cycle Power Plants Configurations Burning Blast Furnace Gas
  61. Performance Evaluation of a Hydraulic Turbine Used As a Turbodrill for Oil and Gas Applications in Post-Salt Environment
  62. 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
  63. Numerical investigation of a HPT with different rotor tip configurations in terms of pressure ratio and efficiency
  64. Combined Cycle Performance Evaluation and Dynamic Response Simulation
  65. Characterization of an ethanol fueled heavy-duty engine powering a generator set
  66. Implicit
  67. Study and Analysis of a Power Turbine Preliminary Design for a Small Turboshaft
  68. One Stage Power Turbine Preliminary Design and Analysis
  69. Gas Turbine Course’s Teaching Process at Instituto Tecnológico de Aeronáutica: Theory and Laboratory
  70. Experiences on Project-Based-Classes for Turbomachine Design in an Aerospace Engineering Undergraduate Program
  71. Evaluation of Different Squealer Cavity Configurations in a HPT Blade Tip Region and its Influence on the Heat Transfer
  72. A Step Further on the Control of Acceleration of Gas Turbines With Controlled Variable Geometry and Combustion Emissions
  73. Technical evaluation of vehicle ignition systems: conduct differences between a high energy capacitive system and a standard inductive system
  74. A Study of the Heat Transfer in Winglet and Squealer Rotor Tip Configurations for a Non-Cooled HPT Blade Based on CFD Calculations
  75. The Flow Machines Course at the Technological Institute of Aeronautics for Mechanical-Aeronautical Engineering Undergraduate Course
  76. Gas Turbine Transients With Controlled Variable Geometry
  77. Performance Evaluation of a 5 kN Gas Turbine Based on Specially Designed Components
  78. Numerical Tools for High Performance Axial Compressor Design for Teaching Purpose
  79. Comparison Between Unstructured and Structured Meshes With Different Turbulence Models for a High Pressure Turbine Application
  80. An Axial Flow Compressor for Operation With Humid Air and Water Injection
  81. Influence of Variable Geometry Transients on the Gas Turbine Performance
  82. Performance Study of a 1 MW Gas Turbine Using Variable Geometry Compressor and Turbine Blade Cooling
  83. An Axial-Flow Compressor for Operation With Humid Air and Water Injection
  84. An Object-Oriented Parallel Finite-Volume CFD Code
  85. Nacelle Design for Mixed Turbofan Engines
  86. Gas Turbine Performance Simulation Using an Optimized Axial Flow Compressor