Towards modeling and simulation of particulate interactions with high-speed transitional boundary-layer flows

O. M.F. Browne, S. M.A. Al Hasnine, C. Brehm

Producción científica: Conference contributionrevisión exhaustiva

16 Citas (Scopus)

Resumen

This paper presents a numerical approach to simulate particulate interactions with high-speed transitional boundary-layer flows. A particle solver is used to simulate the trajectory of particulates, and the solver is coupled via a particulate-flow interaction source term to a nonlinear disturbance flow solver based on the compressible Navier-Stokes equations. To efficiently simulate the particulate flow interactions, an adaptive mesh refinement approach is utilized. 2-D and 3-D particulate flow simulation results are presented. The flow conditions for the 2-D simulations were chosen such that 2-D second-mode instability waves are most amplified, and the frequency range of the disturbances introduced by the particulate collision falls within the unstable frequency range. Although the 2-D simulations were mainly used to test out our new simulation approach, some basic physics were also explored, such as the effect of the particulate size and the impingement location, on the generated disturbance flow field. For the 3-D simulations, two different flow conditions were considered: (1) a M=5.35 flat plate boundary-layer flow where 2-D second-mode instability waves are most amplified, and comparison data from established pulse simulations are available and (2) a M=4 14 degree wedge where 3-D first-mode instability waves are most amplified, and comparison data from other particulate-flow interaction simulations are available. The main purpose of this work is to introduce and validate our adaptive mesh refinement based particulate-flow interaction simulation approach.

Idioma originalEnglish
Título de la publicación alojadaAIAA Aviation 2019 Forum
Páginas1-21
Número de páginas21
DOI
EstadoPublished - 2019
EventoAIAA Aviation 2019 Forum - Dallas, United States
Duración: jun 17 2019jun 21 2019

Serie de la publicación

NombreAIAA Aviation 2019 Forum

Conference

ConferenceAIAA Aviation 2019 Forum
País/TerritorioUnited States
CiudadDallas
Período6/17/196/21/19

Nota bibliográfica

Publisher Copyright:
© 2019 by the American Institute of Aeronautics and Astronautics, Inc.

Financiación

This research is part of the Blue Waters sustained-petascale computing project, which is supported by the National Science Foundation (awards OCI-0725070 and ACI-1238993) and the state of Illinois. Blue Waters is a joint effort of the University of Illinois at Urbana-Champaign and its National Center for Supercomputing Applications. Some funding support was provided by the Office of Naval Research under contract N00014-19-1-2223 with Dr. Eric Marineau as program manager is gratefully acknowledged. Finally, the authors want to thank Dr. Anatoli Tumin at University of Arizona for many fruitful discussions on this topic.

FinanciadoresNúmero del financiador
National Science Foundation (NSF)OCI-0725070, ACI-1238993
Office of Naval ResearchN00014-19-1-2223
University of Illinois, Urbana-Champaign

    ASJC Scopus subject areas

    • Computer Science Applications
    • Electrical and Electronic Engineering
    • Aerospace Engineering

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