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Theoretical Performance Analysis of a Variable Exit-Area Rocket Nozzle for Altitude Adaptation

Fuente: Zenodo

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Dettagli Bibliografici
Autore principale:	GAWALI, Chinmay
Natura:	Recurso digital
Lingua:	inglese
Pubblicazione:	Zenodo 2025
Soggetti:	Aerospace engineering rocket nozzle variable area nozzle altitude adaptation compressible flow nozzle expansion thrust coefficient
Accesso online:	Acceder al recurso
Tags:	Aggiungi Tag Nessun Tag, puoi essere il primo ad aggiungerne!!

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