Mid-fidelity NATO generic destroyer static and moving-ship airwake simulations using the Lattice-Boltzmann method compared with experimental data-Reference-Cited by-同舟云学术

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Mid-fidelity NATO generic destroyer static and moving-ship airwake simulations using the Lattice-Boltzmann method compared with experimental data

Published:2024-04 Issue: Volume:298 Page:117264
ISSN:0029-8018
Container-title:Ocean Engineering
language:en
Short-container-title:Ocean Engineering

Author:

Ashok Shreyas G.^ORCID,Rauleder Juergen^ORCID

Funder

Office of Naval Research

Computer and Information Science and Engineering Office of Advanced Cyberinfrastructure

National Science Foundation Division of Graduate Education

Naval Air Warfare Center Aircraft Division

U.S. Navy

National Science Foundation

Publisher

Elsevier BV

Reference38 articles.

1. A model for collision processes in gases. I. Small amplitude processes in charged and neutral one-component systems;Bhatnagar;Phys. Rev.,1954

2. Bludau, J., Hajek, M., Rauleder, J., 2021. Solving the Ship-Rotorcraft Dynamic Interface Problem Using Lattice-Boltzmann Aerodynamics Two-Way Coupled with Blade Element Based Flight Dynamics. In: Vertical Flight Society Forum 77. Virtual.

3. Momentum transfer of a Boltzmann-lattice fluid with boundaries;Bouzidi;Phys. Fluids,2001

4. The permeability of a random medium: Comparison of simulation with theory;Cancelliere;Phys. Fluids A,1990

5. Improved wall model treatment for aerodynamic flows in LBM;Degrigny;Comput. & Fluids,2021

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