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# Author: A. Da Ronch
#  Email: A.Da-Ronch@soton.ac.uk
#   Date: 21 Dec 2016
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This folder collects the indicial response to a sharp-edge gust obtained using 
the analytical formulation and computed using the DLR-Tau and SU2 CFD solvers. 
All files are in ASCII format and compatible with Tecplot post-processing. 
Filenames follow the convention:

	seg_SRC_mXX_arYY_sZZ.plt

where 

	-SRC defines the methodology: 'ana' (analytical), 'tau' (DLR-Tau) and 'su2' 
	(SU2)
	-XX defines the Mach number: 03 (0.3), 05 (0.5) and 07 (0.7)
	-YY defines the aspect ratio: 08 and 20
	-ZZ defines the wing sweep angle: 00 (0 deg) and (30 deg)
