Prediction of Flow Separation and Side-loads in Rocket Nozzle Using Large-eddy Simulation-Reference-Cited by-同舟云学术

Prediction of Flow Separation and Side-loads in Rocket Nozzle Using Large-eddy Simulation

Published:2020-07-07 Issue:7-8 Volume:34 Page:622-632
ISSN:1061-8562
Container-title:International Journal of Computational Fluid Dynamics
language:en
Short-container-title:International Journal of Computational Fluid Dynamics

Author:

Daviller Guillaume¹^ORCID,Dombard Jérôme¹,Staffelbach Gabriel¹,Herpe Julien²,Saucereau Didier³

Affiliation:

1. Centre Européen de Recherche et de Formation Avancée en Calcul Scientifique, Toulouse, France

2. Centre National d'Études Spatiales, Paris, France

3. ArianeGroup, Vernon, France

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics

Link

https://www.tandfonline.com/doi/pdf/10.1080/10618562.2020.1786540

Reference30 articles.

1. Non-stationary shock motion unsteadiness in an axisymmetric geometry with pressure gradient

2. Wall Pressure Unsteadiness and Side Loads in Overexpanded Rocket Nozzles

3. Babinsky, H., and J.K. Harvey. 2011. Shock Wave-Boundary-Layer Interactions. Cambridge Aerospace Series. Cambridge: Cambridge University Press, 2011.

4. Entropy generation minimization: The new thermodynamics of finite‐size devices and finite‐time processes

5. Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions

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