Assessment of predictive capabilities for aerodynamic heating in hypersonic flow

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Assessment of predictive capabilities for aerodynamic heating in hypersonic flow

Knight, Doyle / Chazot, Olivier / Austin, Joanna / Badr, Mohammad Ali / Candler, Graham / Celik, Bayram / Rosa, Donato de / Donelli, Raffaele / Komives, Jeffrey / Lani, Andrea / ... [mehr]

Abstract

AbstractThe capability for CFD prediction of hypersonic shock wave laminar boundary layer interaction was assessed for a double wedge model at Mach 7.1 in air and nitrogen at 2.1MJ/kg and 8MJ/kg. Simulations were performed by seven research organizations encompassing both Navier-Stokes and Direct Simulation Monte Carlo (DSMC) methods as part of the NATO STO AVT Task Group 205 activity. Comparison of the CFD simulations with experimental heat transfer and schlieren visualization suggest the need for accurate modeling of the tunnel startup process in short-duration hypersonic test facilities, and the importance of fully 3-D simulations of nominally 2-D (i.e., non-axisymmmetric) experimental geometries.

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Dokumentinformationen

Titel :

Assessment of predictive capabilities for aerodynamic heating in hypersonic flow

Beteiligte:

Knight, Doyle (Autor:in) / Chazot, Olivier (Autor:in) / Austin, Joanna (Autor:in) / Badr, Mohammad Ali (Autor:in) / Candler, Graham (Autor:in) / Celik, Bayram (Autor:in) / Rosa, Donato de (Autor:in) / Donelli, Raffaele (Autor:in) / Komives, Jeffrey (Autor:in) / Lani, Andrea (Autor:in)

Erschienen in:

Progress in Aerospace Sciences ; 90 ; 39-53

Erscheinungsdatum :

2017-02-06

Format / Umfang :

15 pages

ISSN :

0376-0421

DOI :

https://doi.org/10.1016/j.paerosci.2017.02.001

Medientyp :

Aufsatz (Zeitschrift)