About Sphere
Overview
A precision sphere model designed for transonic and supersonic wind tunnel testing, ideal for baseline drag studies, flow symmetry validation, and calibration applications. Available in multiple diameters to match test section size, the sphere provides repeatable and well-characterized aerodynamic behavior.
Key Features
- Simple Geometry: Ideal for baseline and validation studies
- Multiple Sizes: Scaled to suit various test sections
- Optional Pressure Instrumentation: Configurable tap locations
- Sting Mounted: Threaded base for quick installation
- High-Precision Manufacturing
Technical Datasheet (Typical)
Geometry
- Model Type: Sphere
- Diameter Range: 25 mm to 300 mm (customizable)
- Surface Finish: Smooth, aerodynamic-grade
Mounting
- Type: Sting-mounted
- Connection: Threaded base for secure and repeatable positioning
Instrumentation
- Standard: Solid sphere (no taps)
- Optional:
- Pressure taps (quantity based on diameter)
- Internal routing for pressure measurement
Performance
- Mach Range: 0.8 to 3.0+ (application dependent)
- Use Case: Drag benchmarking and flow uniformity checks
- Repeatability: High due to symmetric geometry
Optional Features
- Multi-point pressure measurement system
- Custom diameters and materials
- Surface coatings or finishes
- Handcrafted custom models and probes
Applications
- Wind tunnel calibration and validation
- Drag coefficient benchmarking
- Flow uniformity and symmetry studies
- Educational and research experiments
Customization
Each sphere model can be custom-built to match specific tunnel sizes, instrumentation needs, and research objectives.