A Parallel Adaptive Newton-Krylov-Schwarz Method for 3D Compressible Inviscid Flow Simulations

Table 1

X29 aircraft. Time for successive adaptations using 8 and 16 processors.

		78 secs.	Grid derefinement/refinement
First cycle 𝒯^(1); 2 cycles	𝑀=8	690 secs.	Regularisation and optimisation
		132 secs.	Overheads
		854 secs.	Grid derefinement/refinement
Final Grid 𝒯^(3); 2 cycles	𝑀=16	2860 secs.	Regularisation and optimisation
		1002 secs.	Overheads