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Theoretical Performance Analysis of a Variable Exit-Area Rocket Nozzle for Altitude Adaptation
Theoretical Performance Analysis of a Variable Exit-Area Rocket Nozzle for Altitude Adaptation
Fuente:
Zenodo
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Bibliographic Details
Main Author:
GAWALI, Chinmay
Format:
Recurso digital
Language:
English
Published:
Zenodo
2025
Subjects:
Aerospace engineering
rocket nozzle
variable area nozzle
altitude adaptation
compressible flow
nozzle expansion
thrust coefficient
Online Access:
Acceder al recurso
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Internet
https://doi.org/10.5281/zenodo.17771692
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