Verification Study of Locally Partitioned Interpolation Method for Patched-Grid Algorithm
Author:
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s42405-022-00529-5.pdf
Reference25 articles.
1. Bohbot J, Bertin D, Darraq D (2000) A conservative patched grid algorithm for turbulent flow computations of 3d complex aircraft configurations. In: European Congress on Computational Methods in Applied Sciences and Engineering
2. Hessenius KA, Rai MM (1986) Three-dimensional, conservative, Euler computations using patched grid systems and explicit methods. In: 4th Joint Fluid Mechanics, Plasma Dynamics and Lasers Conference
3. Holst T, Kaynak U, Gundy K, Thomas S, Flores J, Chaderjian N (1985) Numerical solution of transonic wing flows using an Euler/Navier-Stokes zonal approach. In: 18th Fluid Dynamics and Plasma Dynamics and Lasers Conference
4. Chen H, Fu S, Li FW (2003) Navier-Stokes simulations for transport aircraft wing/body high-lift configurations. J Aircr 40(5):883–890. https://doi.org/10.2514/2.6878
5. Rai MM (1986) A conservative treatment of zonal boundaries for Euler equation calculations. J Comput Phys 62(2):472–503. https://doi.org/10.1016/0021-9991(86)90141-5
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