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

Author/s: Fernández Torres, Christopher Fernando
Advisor/s: Pax Dolz Del Castellar, Rafael
Keyword/s: Diseño peliminar; Tobera de área variable; Postcombustion; Ciclo de motor; Análisis multifísico
Degree: Grado en Ingeniería Aeroespacial en Aeronaves
Date of defense: 2024-06
Type of content: TFG
URI: https://hdl.handle.net/20.500.12880/8418
Abstract:
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.
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