Clark Y-14 Slat/Flap Wing

About Clark Y-14 Slat/Flap Wing

Overview

A precision airfoil test model based on the Clark Y-14 profile, featuring infinitely adjustable slats and flaps for advanced high-lift and flow control studies. Designed for compatibility with standard sting balances, the model supports both flow visualization and aerodynamic force measurements.

Key Features

• Infinitely Adjustable Slats & Flaps for high-lift configuration studies
• Clark Y-14 Airfoil Profile for realistic aerodynamic behaviour
• Dual Use: Suitable for visualization and force testing
• Standard Mounting: Compatible with 3/8-inch string balances
• Compact, High-Precision Construction

Technical Datasheet (Typical)

Geometry

• Airfoil Type: Clark Y-14
• Span: 250 mm (9.875 in)
• Chord: 90 mm (3.5 in)
• Configuration: Slat and flap adjustable system

Mounting

• Type: Sting-mounted
• Compatibility: 3/8-inch sting balance

Adjustability

• Slat Angle: Continuously variable
• Flap Angle: Continuously variable

Performance

• Application Range: Low-speed to moderate-speed wind tunnel testing
• Use Case: Lift enhancement, stall behaviour, and flow separation studies
• Measurement Compatibility: External/internal force balances

Optional Features

• Integrated pressure taps
• Angle measurement scales or digital readouts
• Custom airfoil profiles and sizes
• Handcrafted custom models and probes

 Applications

• High-lift device research
• Stall and flow separation analysis
• Aerodynamic coefficient measurement
• Educational demonstrations and lab experiments

Customization

Available as a fully customizable model, allowing adjustments in size, airfoil profile, and instrumentation to meet specific research needs.