The GUNT HM 170.21 Aerofoil with Slat and Slot Flap is designed for use in the measuring section of the HM 170 wind tunnel to study flow around bodies. The aerofoil model features an adjustable slat and an adjustable slot flap at the rear. The slat separation to the leading edge of the base profile can be varied, while the slot flap can be adjusted in angle and separation or detached entirely. The base profile with the slat corresponds to the symmetrical NACA 0015 profile. Circular covering discs prevent secondary flows. The aerofoil is placed in the force sensor to measure the drag force acting on it.
Product Features
- Used in the measuring section of the HM 170 wind tunnel
- Features an adjustable slat and adjustable slot flap at the rear
- Slat separation to the leading edge and slot flap angle/separation can be varied
- Slot flap can be detached
- Base profile corresponds to symmetrical NACA 0015 profile
- Circular covering discs prevent secondary flows
- Placed in the force sensor to measure drag force
Benefits
- Enables precise study of aerofoil flow characteristics with adjustable slat and flap
- Supports aerodynamic experiments with variable geometry settings
- Prevents secondary flows for accurate drag measurement
- Durable construction ensures repeated use in teaching and research
Why Choose GUNT HM 170.21 - Aerofoil with Slat and Slot Flap?
The GUNT HM 170.21 Aerofoil with Slat and Slot Flap allows detailed drag force studies in the HM 170 wind tunnel, supporting flexible aerodynamic experiments with adjustable slat and flap settings.
