Comparison of Frequency Domain and Time-Domain Methods for Aeromechanical Analysis

Table 1

Geometric parameters and flow conditions for the flat plate test case.

True chord length	0.1 m
Stagger angle	= 45°
Pitch/chord ratio	1
Span/chord ratio	3
Steady incidence	0
Steady Mach number	0.7
Reduced frequency	1
Interblade phase angle	0, 180