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Trisonic Wind Tunnel

Name: Trisonic Wind Tunnel
Brand: MECHMATICS ENGINEERING PVT. LTD.
Price: 500000.0 INR
Availability: InStock

Price 500000.0 INR/ Number

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MOQ : 1 Number

Trisonic Wind Tunnel Specification

Equipment Type
Wind Tunnel

Material
Mild Steel

Processing Type
Mechanical

Condition
New

Technology
Trisonic (Subsonic, Transonic, Supersonic)

Dimension (L*W*H)
Customized as per client requirement

Power Mode
Electric

Voltage
220V - 440V

Power Consumption
Ac Motor Driven, varies by model

Pressure Output
Adjustable

Application
Aerospace and Research Laboratories

Coating Type
Epoxy Coated

Accessories
Control Panel, Data Acquisition System, Model Support

Safety Feature
Emergency Stop, Overload Protection

Max Test Model Size
Configurable

Working Speed
Up to Mach 4.0

Installation Type
Stationary

Data Output
Digital

Control Type
PLC Controlled

Observation Window
Acrylic, Impact Resistant

Cooling System
Forced Air

Noise Level
<85 dB

Test Section Size
Typically 200 mm x 200 mm

About Trisonic Wind Tunnel

Short Marketing Overview

Our Trisonic Wind Tunnel System is a versatile, high-performance aerodynamic testing facility designed to cover subsonic, transonic, and supersonic regimes within a single platform. Engineered for precision and flexibility, the system enables seamless Mach number control using adaptive nozzle and diffuser technologies, ensuring high-quality flow conditions across all speed ranges.

With advanced boundary-layer control, excellent optical access, and modular model mounting configurations, this system supports both fundamental research and industrial development, making it ideal for aerospace, automotive, and structural aerodynamics applications.

Technical Datasheet (Generalized Ranges)

Flow Performance

Mach Number Range: 0.3 3.5
Mach Number Accuracy: 0.003 to 0.01
Dynamic Pressure Range: 1 6 bar
Pressure Accuracy: 3 10 mbar

Test Section

Typical Dimensions:

Length: 1.5 2.5 m
Width: 0.3 1.0 m
Height: 0.5 1.5 m

Configuration: Rectangular / customizable
Optical Access: Multi-window (high optical clarity)
Wall Type:

Solid + suction-assisted (transonic regime)

Angle of Attack Range: 10 to +40

Flow Control System

Subsonic Control: Adjustable diffuser system
Supersonic Control: Variable geometry Laval nozzle
Transonic Control:

Wall suction / boundary layer control
Adjustable plenum chamber & wall geometry

Pressure & Storage System

Pressure Reservoir Volume: 100 500 m
Maximum Storage Pressure: up to 20 30 bar
Fill Time: ~60 120 minutes (depending on system size)

Nozzle & Geometry

Nozzle Contraction Ratio: 5 10
Type: Adjustable / interchangeable contour nozzles
Diffuser: Variable geometry for efficient flow recovery

Test Duration

Blowdown Operation: 10 60 seconds (typical, depending on conditions)

Reynolds Number

Typical Range: 110 110 per meter
Adjustable via pressure and Mach control

Measurement & Instrumentation

Force & Pressure Measurement:

Static pressure sensors (10100 Hz)
Dynamic pressure sensors (up to 100 kHz)

Flow Diagnostics:

Particle Image Velocimetry (PIV)
Pressure-Sensitive Paint (PSP)
Infrared thermography
Schlieren / shadowgraph systems

Structural Measurement:

Deformation / strain measurement systems

Model Mounting Options

Rear sting mount
Side-wall mounting
Floor / ceiling mounting
Custom modular fixtures

Key Features

Single facility for multi-regime testing (subsonic to supersonic)
Advanced boundary layer suction system for transonic flow quality
High flow uniformity and repeatability
Flexible test section and mounting configurations
Suitable for large and instrumented models

Applications

Aircraft and UAV aerodynamic testing
Missile and high-speed vehicle development
Automotive aerodynamics
Structural wind engineering (bridges, buildings)
Fundamental aerodynamics research

Advanced Trisonic Technology

This wind tunnel integrates trisonic capabilities, allowing for seamless transitions between subsonic, transonic, and supersonic speeds up to Mach 4.0. Controlled by a reliable PLC system, researchers and engineers can simulate a wide range of aerodynamic scenarios, supporting comprehensive experimental needs.

User-Centric Design & Safety

With a clear, impact-resistant acrylic observation window and easy-to-configure test model support, the Trisonic Wind Tunnel ensures safe and adaptable operation. The inclusion of an emergency stop and overload protection prioritizes operator safety, while digital data output and a modern control panel streamline data collection and experiment management.

Versatile Applications & Customization

Designed for aerospace and research laboratories, this equipment accommodates various testing requirements with its adjustable pressure output, customizable model size, and tailored dimensions. Its epoxy coating and forced air cooling system guarantee longevity and operational reliability in demanding environments.

FAQ's of Trisonic Wind Tunnel:

Q: How does the Trisonic Wind Tunnel operate across different speed regimes?

A: The Trisonic Wind Tunnel is engineered to operate seamlessly across subsonic, transonic, and supersonic regimes, achieving speeds up to Mach 4.0. A PLC-based control system manages airflow conditions, allowing users to switch between regimes as required by the research or test scenario.

Q: What types of experiments or tests can be conducted using this wind tunnel?

A: This wind tunnel is designed for a variety of aerodynamic experiments, particularly in aerospace and research laboratory settings. Researchers can test scale models, assess aerodynamic forces, visualize flow patterns, and gather digital data for analysis across trisonic speed ranges.

Q: When is it necessary to utilize the emergency stop or overload protection features?

A: Emergency stop and overload protection should be activated in the event of unexpected operational anomalies, equipment malfunction, or to prevent potential hazard to personnel or the tested model. These safety features are especially critical when testing at high speeds or with high-pressure outputs.

Q: Where can observation and data recording take place during testing?

A: Operators can observe model behavior in real-time through the acrylic, impact-resistant observation window in the test section. Digital data output, collected via the data acquisition system, is accessible from the control panel, allowing for remote monitoring and recording during tests.

Q: What is the process for installing and configuring this wind tunnel for a specific application?

A: The installation involves positioning the stationary wind tunnel as per lab requirements. Key parameters like test model size, pressure output, and dimensions are customized during setup. Model supports and accessories are configured to accommodate specific experimental setups, ensuring optimal test conditions.

Q: How does the forced air cooling system contribute to tunnel performance?

A: The forced air cooling system prevents overheating of mechanical components during high-speed operations. This ensures stable performance, prolongs equipment lifespan, and allows experiments to run without thermal-related interruptions.

Q: What benefits does the digital data output provide to researchers?

A: Digital data output streamlines data collection, minimizing manual intervention and errors. Researchers benefit from real-time monitoring, precise data logging, and easier post-processing of aerodynamic measurements, facilitating more accurate and efficient analyses.

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