@misc{20.500.12880/8418,
year = {2024},
month = {6},
url = {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.},
title = {Preliminary Design Of A Variable Area Propelling Nozzle For An Afterburning Military Aircraft Engine},
keywords = {Diseño peliminar},
keywords = {Tobera de área variable},
keywords = {Postcombustion},
keywords = {Ciclo de motor},
keywords = {Análisis multifísico},
author = {Fernández Torres, Christopher Fernando},
}