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

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Aircraft Hydraulic System

Aircraft Hydraulic System Continue reading

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Flight control surfaces

Flight control surfaces Continue reading

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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 – Combustion … Continue reading

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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

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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

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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

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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

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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

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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

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