Towards Detached-Eddy Simulation of Flow Around Rotorcraft Using Immersed Boundary Method-Reference-Cited by-同舟云学术

Towards Detached-Eddy Simulation of Flow Around Rotorcraft Using Immersed Boundary Method

Published:2020-11 Issue:11 Volume:58 Page:4893-4907
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Park Hee Sung¹,Linton Daniel¹,Thornber Ben¹

Affiliation:

1. University of Sydney, Sydney, New South Wales 2006, Australia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference35 articles.

1. Coupling of an Unsteady Aerodynamics Model with a Computational Fluid Dynamics Solver

2. An Immersed-Boundary Finite-Volume Method for Simulations of Flow in Complex Geometries

3. BrandA. G.KomerathN. M.McMahonH. M. “Wind Tunnel Data from a Rotor Wake/Airframe Interaction Study,” Georgia Inst. of Technology TR DAAG29-82-K-0094, Atlanta, GA, 1986.

4. BrandA. G. “An Experimental Investigation of the Interaction Between a Model Rotor and Airframe in Forward Flight,” Ph.D. Thesis, Georgia Inst. of Technology, Atlanta, GA, 1989.

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