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Products  |  Fluid Mechanics and Hydrology  |  Fundamentals of Aerodynamics and Airflow  |  HM 170  |  HM 170.21
HM 170.21 Aero Foil with Flap and Slot Show data sheet (pdf file) Print page
Technical Description
The HM 170.21 Aerofoil with Flap and Slot has an adjustable slat and an adjustable slot flap on the rear. On the slat it is possible to vary the separation to the leading edge of the base profile; the slot flap can be adjusted in angle and separation. Together with the slat, the base profile of the aerofoil corresponds to the symmetrical profile NACA 15. To avoid secondary flows, the aerofoil is fitted with circular covering discs. The model is places in a 2-component force transducer, this outputs the drag and lift forces acting on the body in the flow as measured values.
Learning Objectives / Experiments
Experiments on bodies in flows
Influence of a slat
Influence of a slot flap
Features
Aerofoil model for investigating aerodynamic lift aids
Specification
[1] Model with slat and flap for investigating the influence of control surfaces on aerofoils
[2] Aerofoil with slat profile NACA 15, lxwxh 100x100x15mm
[3] Force transducer section up to the middle of the model 239mm
Technical Data
Profile: NACA 15
Dimensions and Weight
l x w x h: 116 x 116 x 299 mm
Weight : ca. 0,7 kg
Scope of Delivery
1 aerofoil model, 1 instruction manual
Order Details
070.17021 HM 170.21 Aero Foil with Flap and Slot
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