Technology
TUPAN 1000
PROPULSION TF-300 / Turbofan
Tupan Propulsion TF-300 is a turbofan engine, composed by a fan-compressor rotor driven by a two-stages turbine, and a direct flux annular combustion chamber.
TECHNICAL SPECIFICATION
Fan – Axial Single stage
Compressor: Diagonal Single-stage
Combustors: Annular
Turbine: two-stages axial
Dimension
Length: 420 mm
Diameter: 250 mm
Dry weight: 16 kg
Performance
Thrust: 300lbf
SFC: 0,9 kg/Kgf/h
TUPAN 2000
PROPULSION TF-700 / Turbofan
Tupan Propulsion TF-700 is a turbofan engine, composed by a fan-compressor rotor driven by a two-stages turbine, and a direct flux annular combustion chamber.
TECHNICAL SPECIFICATION
Fan – Axial Single stage
Compressor: One axial stage and one diagonal single-stage
Combustors: Annular
Turbine: two-stages axial
Dimension
Length: 580 mm
Diameter: 300 mm
Dry weight: 45 kg
Performance
Thrust: 700lbf
SFC: 0,85 kg/Kgf/h
TUPAN 3000
PROPULSION TF-1200 / Turbofan
Tupan Propulsion TF-1200 is a turbofan engine, composed by a fan-compressor rotor driven by a two-stages turbine, and a direct flux annular combustion chamber.
TECHNICAL SPECIFICATION
Fan – Axial Single stage
Compressor: One axial stage and one diagonal single-stage
Combustors: Annular
Turbine: Two axial stages
Dimension
Length: 960 mm
Diameter: 350 mm
Dry weight: 86 kg
Performance
Thrust: 1200lbf
SFC: 0,8 kg/Kgf/h
TUPAN 4G Simulation
The application of CFD to aircraft design configurations and its influence on the aircraft development and support process is analyzed.
Results indicate that combining CFD and the wind tunnel can achieve design solutions that otherwise would not be found, and can also significantly reduce the length of the design cycle.
It is concluded that CFD provides for a better understanding of flow physics, achievement of design solutions that are otherwise unobtainable, and reduction of development flowtime.
