Tag Archives: compression

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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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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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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