Hypersonic aerodynamics of a deformed aeroshell in continuum and near-continuum regimes

The flexible inflatable aeroshell naturally deforms under aerodynamic loads during atmospheric entry. In this paper, we investigate the hypersonic aerodynamics of an inflatable aeroshell forebody with undulated surface deformation in the continuum and near-continuum flow regimes, where flow physics...
Ausführliche Beschreibung

Gespeichert in:
Autor*in:

Guo, Jinghui [verfasserIn]

Lin, Guiping [verfasserIn]

Zhang, Jun [verfasserIn]

Bu, Xueqin [verfasserIn]

Li, Hao [verfasserIn]

Format:

E-Artikel

Sprache:

Englisch

Erschienen:

2019

Schlagwörter:

Aerodynamic analysis

Surface deflection

Slip boundary condition

Hypersonic flow

Computational fluid dynamics

Übergeordnetes Werk:

Enthalten in: Aerospace science and technology - Amsterdam [u.a.] : Elsevier Science, 1997, 93

Übergeordnetes Werk:

volume:93

DOI / URN:

10.1016/j.ast.2019.07.029

Katalog-ID:

ELV002950618

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