Turbofan – Introduction
1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4 –
Turbogas cycle
1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4
Performance of Jet Engine
1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4
Aerodinamic for compressible gas
1 – Introduction 2 – Aerodinamic for compressible gas – Basic principles 3 – Performance of Jet Engine 4 –
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:
Lability and hyperstaticity of a structure
A structure is labile if is possible to have a rigid cinematism, it is isostatic if is possible to calculate
Preliminary sizing – Matching Chart
Introduction This article introduces the first step in the preliminary sizing process, which is to determine the so-called aircraft
Random Vibration Analysis – Nastran SOL 111
Introduction Random vibration is motion which is non-deterministic, meaning that future behavior cannot be precisely predicted, and