The GUNT HM 170.27 Pressure Distribution on an Aerofoil NACA 4415 is designed for use in the HM 170 wind tunnel to record the pressure distribution on an aerofoil profile. The aerofoil is mounted in the wind tunnel’s two-component force sensor, and the angle of attack can be varied by rotating the mount. The surface of the aerofoil is fitted with measuring holes arranged to minimize mutual interaction, with each point connected to a hose. Two side panels enclose the aerofoil to prevent secondary flows. Static pressures are displayed using tube manometers HM 170.50 or via electronic pressure measurement HM 170.55.
Product Features
- Used in the HM 170 wind tunnel for aerofoil pressure distribution studies
- Aerofoil profile: NACA 4415
- Angle of attack adjustable via rotating mount
- Surface fitted with measuring holes arranged to minimize interaction
- Each measuring point connected to a hose for pressure recording
- Enclosed by side panels to prevent secondary flows
- Static pressures displayed via tube manometers HM 170.50 or electronic measurement HM 170.55
Benefits
- Enables precise study of pressure distribution over an aerofoil
- Supports aerodynamic research and teaching applications
- Minimizes interaction between measurement points for accurate readings
- Flexible pressure display options for experiments and analysis
Why Choose GUNT HM 170.27 - Pressure Distribution on an Aerofoil NACA 4415?
The GUNT HM 170.27 Pressure Distribution on an Aerofoil NACA 4415 allows detailed investigation of aerofoil aerodynamics in the HM 170 wind tunnel, supporting research, education, and precision measurements.
