Preliminary Design Of A Variable Area Propelling Nozzle For An Afterburning Military Aircraft Engine

Fernández Torres, Christopher Fernando

Autor/es: Fernández Torres, Christopher Fernando

Director/es: Pax Dolz Del Castellar, Rafael

Palabra/s clave: Diseño peliminar; Tobera de área variable; Postcombustion; Ciclo de motor; Análisis multifísico

Titulación: Grado en Ingeniería Aeroespacial en Aeronaves

Fecha de defensa: 2024-06

Tipo de contenido: TFG

URI: https://hdl.handle.net/20.500.12880/8418

Resumen:

This project presents the peliminary design of a variable area propelling nozzle for an afterburning military aircraft engine. The study begins with an engine cycle analysis using a Python script to interate through various flight speeds and altitudes, simulating engine performance with and without afterburners.