A Comparative Performance Analysis of the Novel TurboAux Engine with a Turbojet Engine, and a Low-Bypass Ratio Turbofan Engine with an Afterburner
Description
Toolbox-ID
jz000097-0024
Identifier(s)
https://tustorage.ulb.tu-darmstadt.de/handle/tustorage/9582
Publisher
MDPI AG
License
https://creativecommons.org/licenses/by/4.0/
Subject(s)
DDC(s)
620