Category Archives: Aircraft Design
Operating Flight Strength (V-g / V-n Diagrams – Maneuver Speed)
In aerodynamics, the flight envelope defines operational limits for an aerial platform with respect to maximum speed and load factor given a particular atmospheric density. The flight envelope is the region within which an aircraft can operate safely. The V-g diagram … Continue reading
Engine Inlet Ducts
1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4 – Turbogas cycle 5 – Turbofan 5.1 Turbofan with separated flows 5.2 Turbofan with associated flows 6 – … Continue reading
Turbofan – Introduction
1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4 – Turbogas cycle 5 – Turbofan 5.1 Turbofan with separated flows 5.2 Turbofan with associated flows 6 – Combustion … Continue reading
Turbofan
1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4 – Turbogas cycle 5 – Turbofan 5.1 Turbofan with separated flows 5.2 Turbofan with associated flows 6 – Combustion … Continue reading
Turbogas cycle
1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4 – Turbogas cycle 5 – Turbofan 5.1 Turbofan with separated flows 5.2 Turbofan with associated flows 6 – … Continue reading
Performance of Jet Engine
1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4 – Turbogas cycle 5 – Turbofan 5.1 Turbofan with separated flows 5.2 Turbofan with associated flows 6 – … Continue reading
Aerodinamic for compressible gas
1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4 – Turbogas cycle 5 – Turbofan 5.1 Turbofan with separated flows 5.2 Turbofan with associated flows 6 – Combustion … Continue reading
Verifying of a fuselage frame symmetrically loaded
The fuselage frame is a principal structural element of the aircraft shell structure, it is important for the following reasons: ensuring a certain shape to the fuselage, establishing an aerodynamic requirements that must be met. Frames used purely to have … Continue reading