IH60 Rotor Blade

@IH_60_SECTION_DEFINITION {
@IH_60_SECTION_NAME {Ih60Name} {
@DIMENSIONS {
@DIMENSION_01 {c}
@DIMENSION_02 {tO}
@DIMENSION_03 {η1T}
@DIMENSION_05 {η2T}
@DIMENSION_05 {tI}
@DIMENSION_06 {η1B}
@DIMENSION_07 {η2B}
@DIMENSION_08 {ηc}
@DIMENSION_09 {α}
@DIMENSION_10 {β}
}
@MATERIALS {
@MATERIAL_01 {Mat1}
@MATERIAL_02 {Mat2}
@MATERIAL_03 {Mat3}
}
@AIRFOIL_SHAPE_NAME {AirfName}
@NUMBER_OF_CONTROL_POINTS {Ncp}
@IS_DEFINED_IN_FRAME {FrameName}
@MESH_DENSITY {md}
@COMMENTS {CommentText}
}
}

Notes

The IH60 rotor blade section: base configuration

Component Dimension Symbol Default Nb.
Airfoil chord length c required 01
Airfoil thickness tO required 02
Airfoil location η1T required 03
Airfoil location η2T required 04
Airfoil thickness tI required 05
Airfoil location η1B η1T 06
Airfoil location η2B η2T 07
Aft core location ηc required 08
Table 1. Dimensions defining the geometry of the IH60 rotor blade section.
Figure 1. The IH60 rotor blade section
Figure 2. The IH60 rotor blade section, inner wrap detail
Figure 4. The IH60 rotor blade section, leading edge detail
Figure 4. The IH60 rotor blade section, trailing edge detail