An efficient finite differences method for the computation of compressible, subsonic, unsteady flows past airfoils and panels.
Manuel ColeraMiguel Pérez-SaboridPublished in: J. Comput. Phys. (2017)
Keyphrases
- high accuracy
- similarity measure
- computational complexity
- significant improvement
- clustering method
- dynamic programming
- experimental evaluation
- computational cost
- high precision
- probabilistic model
- cost function
- prior knowledge
- pairwise
- data sets
- support vector machine
- edge detection
- model selection
- moving objects
- synthetic data
- fully automatic
- highly efficient