Study of Sweep and Induced Dihedral Effects in Subsonic Axial Flow Compressor Passages—Part I: Design Considerations—Changes in Incidence, Deflection, and Streamline Curvature

Table 1

S. No	Scheme	Code
(1)	Unswept rotor	UNS
	(Baseline)
(2)	20^o Forward sweep	20^o TCS
	(Tip chordline swept)
(3)	30^o Forward sweep	30^o TCS
	(Tip chordline swept)
(4)	20^o Forward sweep	20^o AXS
	(Axially swept)
(5)	30^o Forward sweep	30^o AXS
	(Axially swept)