Category Archives: Aircraft Design

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

Posted in Turbofan | Tagged , , | Leave a comment

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

Posted in Turbofan | Tagged , , | Leave a comment

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

Posted in Turbofan | Tagged , , | Leave a comment

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

Posted in Turbofan | Tagged , , | Leave a comment

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

Posted in Turbofan | Tagged , , | Leave a comment

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

Posted in Turbofan | Tagged , , | Leave a comment

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

Posted in Aircraft Design | Tagged , , | Leave a comment

Preliminary sizing – Matching Chart

  Introduction This article introduces the first step in the preliminary sizing process, which is to determine the so-called aircraft design point in terms of wing loading and thrust-to-weight ratio. The requirements, constraints imposed by market, passengers, payload, weight are the factors … Continue reading

Posted in Aircraft Design | Tagged , , , , , , , , , , , , , | Leave a comment

Winglets

Wingtip devices are usually intended to improve the efficiency of fixed-wing aircraft. There are several types of wingtip devices, and although they function in different manners, the intended effect is always to reduce the aircraft’s drag by partial recovery of the tip vortex … Continue reading

Posted in Wing | Tagged , , , , , , , , , , , , , , , , , | Leave a comment