Abstract
A new method developed for immersed boundary problems is presented. With this method, the fluxes through the computational faces are controlled using a so-called “hinge” matrix. The method is simple to implement and is comparable in accuracy to other immersed boundary methods, such as the Cartesian grid method. However, by using the hinge matrix to control the fluxes, complex interpolations are avoided. The Hinge method is verified by solving a low-speed flow in an irregular domain. The verification indicates that spatial accuracy is maintained even when a coarse mesh is used. The method is then applied to multiple CFD problems including flow through obstacles and high-speed channel flow. To further demonstrate the potential, the developed method is then applied to study the conjugate heat transfer, solid sublimation in fluid, and hypersonic fluid-ablation interaction modeling. Numerous applications are presented to show the great potentials of this new method. Results also show that the proposed method provides a convenient way to model general CFD problems without extensive meshing.
| Original language | English |
|---|---|
| Title of host publication | AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021 |
| DOIs | |
| State | Published - 2021 |
| Event | AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021 - Virtual, Online Duration: Aug 2 2021 → Aug 6 2021 |
Publication series
| Name | AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021 |
|---|
Conference
| Conference | AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021 |
|---|---|
| City | Virtual, Online |
| Period | 8/2/21 → 8/6/21 |
Bibliographical note
Publisher Copyright:© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Funding
Financial support for this work was provided by The National Aeronautics and Space Administration Space Technology Research, Development, Demonstration, and Infusion (NASA SpaceTech-REDDI) Award 80NSSC18K0261 and Air Force of Office of Scientific Research 2020 (AFOSR) FA9550-18-1-0261.
| Funders | Funder number |
|---|---|
| National Aeronautics and Space Administration | 80NSSC18K0261 |
| Air Force Office of Scientific Research, United States Air Force | FA9550-18-1-0261 |
ASJC Scopus subject areas
- Aerospace Engineering
- Energy Engineering and Power Technology
- Nuclear Energy and Engineering
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