Blade solidity
Blade solidity is an important design parameter for the axial flow impeller and is defined as the ratio of blade chord length to spacing.
![](../I/m/Wing_profile_nomenclature.svg.png)
- Blade Solidity = c/s
Where
- is the spacing
- is the mean radius
- is blade number
- Chord length c is the length of the chord line
In case of an axial flow impeller mean radius is defined in terms of hub (,inner radius) and tip radius (,outer radius) as :
Blade solidity affects various turbomachinery parameters. So to vary those parameters one needs to vary blade solidity but there are some limitations imposed by Aspect ratio (wing) (span/chord), pitch. If an impeller has few blades i.e high pitch it will result in less lift force and in a similar manner for more blades i.e. very low pitch, there will be high drag force.
Blade solidity should not be confused with rotor solidity, which is the ratio of the total area of the rotor blades to the swept area of the rotor.
Flow over isolated airfoil
Blade solidity is an important parameter that inter relates turbomachine parameter to airfoil parameter. Lift and drag coefficient for an airfoil is inter related to blade solidity as shown:
where
- is lift coefficient
- is the drag coefficient
- is the inlet flow angle on the airfoil
- is the outlet flow angle on the airfoil
- is the mean flow angle
- is inlet flow velocity i.e relative to airfoil
- is mean flow velocity
- is the pressure loss
In an airfoil the mean line curvature is designed to change the flow direction, the vane thickness is for strength and the streamlined shape is to delay the onset of boundary layer separation, taking all the design factors of an airfoil resulting forces of lift and drag can be expressed in terms of lift and drag coefficient.
- b is the wingspan
- c is the chord length
Preliminary design procedure
Design of the impeller depends on specific speed, hub-tip ratio and solidity ratio. To illustrate the dependence, an expression for axial flow pump and fan is shown
where
- is ratio of hub to tip diameter
- is the specific speed
Cordier diagram can be used to determine specific speed and impeller tip diameter . Accordingly solidity ratio and hub-tip ratio (range 0.3-0.7) can be adjusted.
Solidity ratio generally falls in the range of 0.4-1.1
See also
- Aerodynamics
- Turbomachinery
- Axial-flow pump
- Mechanical fan
- Compressors
- Autorotation_(helicopter)
References
- Peng, William W. (2008), Fundamentals of Turbomachinery, Wiley, ISBN 978-0-470-12422-2
- Venkanna, B.K. (2009), Fundamentals of Turbomachinery, PHI learning private limited, ISBN 978-81-203-3775-6
- Turton, R.K. (1995), Principles of turbomachinery, Springer (New Delhi), ISBN 8184896042
- Rama, S.R. Gorla (2003), Turbomachinery Design and Theory, Marcel Dekker ,Inc., ISBN 0-8247-0980-2
- Yahya, S.M. (2002), Turbines, compressors and fans, TMH, ISBN 0070707022