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Design and Analysis of a Base Bleed Unit for the Drag Reduction of a High-Power Rocket Operating at Transonic Speeds

In the present study, a passive flow device is considered for drag reduction purposes through implementation in a transonic high-power rocket. The high-power rocket serves as a reference platform that, apart from the operating conditions, enforces several constraints in terms of available volume and...

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Principais autores: Petros Famellos, Athanasios Skevas, Asterios Koutsiadis, Christos Koutsouras, Pericles Panagiotou
Formato: Artigo
Idioma:Inglês
Publicado em: MDPI AG 2024-05-01
coleção:Aerospace
Assuntos:
base bleed
rocket
wake flow
drag coefficient
base drag
CFD
Acesso em linha:https://www.mdpi.com/2226-4310/11/5/385
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