%0 Thesis
%A Fernández Torres, Christopher Fernando
%8 2024-06
%U https://hdl.handle.net/20.500.12880/8418
%X 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.
%T Preliminary Design Of A Variable Area Propelling Nozzle For An Afterburning Military Aircraft Engine
%K Diseño peliminar
%K Tobera de área variable
%K Postcombustion
%K Ciclo de motor
%K Análisis multifísico
%~ END