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Hypersonic High Enthalpy Wind Tunnel

Name: Hypersonic High Enthalpy Wind Tunnel
Brand: MECHMATICS ENGINEERING PVT. LTD.
Price: 500000.0 INR
Availability: InStock

Price 500000.0 INR/ Unit

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MOQ : 1 Unit

Hypersonic High Enthalpy Wind Tunnel Specification

Equipment Type
Hypersonic High Enthalpy Wind Tunnel

Material
Stainless Steel, High-Grade Alloy Steel, Quartz Windows

Processing Type
Thermal and Fluidic Simulation

Condition
New

Technology
High Enthalpy Plasma Arc Heated Wind Tunnel

Dimension (L*W*H)
Customized (Typical: 8.0 m x 2.5 m x 2.8 m)

Power Mode
Electric

Voltage
380 V - 440 V, 3-Phase AC

Power Consumption
120 kW - 500 kW

Pressure Output
Up to 40 bar

Application
Aerodynamics and Aerospace Research, Hypersonic Vehicle Analysis, Material Testing at High Temperature

Coating Type
Temperature Resistant Ceramic Coating

Accessories
Control Console, Vacuum System, Nozzle Sets, Data Acquisition Modules

Data Output Interface
Ethernet, USB, RS-485

Measurement Systems
Optical Windows, Pressure Sensors, Thermocouple Arrays

Cooling System
Active Water/Glycol Cooling

Compliance Standards
ASTM E2589, ISO 15821

Test Section Diameter
300 mm - 600 mm (Customizable)

Start-Up Time
< 90 minutes

Noise Level
Below 80 dB(A)

Control Method
PLC Based Automated Control System

Chamber Material
High-Temperature Alloy Steel

Maximum Gas Temperature
Up to 5000 K

About Hypersonic High Enthalpy Wind Tunnel

Marketing Overview

The Hypersonic High Enthalpy Wind Tunnel is a specialized testing system designed to replicate the extreme thermal and aerodynamic conditions encountered by high-speed vehicles such as rockets, re-entry bodies, and hypersonic aircraft. By generating high-temperature, high-energy flow, the system enables accurate evaluation of aerodynamic performance, heat transfer, and material behavior under realistic flight conditions.

Ideal for advanced aerospace and defense research, this facility supports critical studies in aerothermodynamics, thermal protection systems, and high-speed propulsion.

Technical Datasheet (Generalized Ranges)

1. System Classification

Type: High-enthalpy / Blowdown / Shock / Arc-heated
Flow Regime: Hypersonic (Mach > 5)

2. Test Section

Shape: Circular / Axisymmetric
Size Range: ~0.1 m 1.0 m
Length: ~0.5 m 3 m

3. Flow Performance

Mach Number Range: ~5 15 (extendable to 20+)
Velocity Range: ~2,000 5,000 m/s
Reynolds Number: ~10 10 per meter
Flow Uniformity: 1% 5%

4. Enthalpy & Thermal Conditions

Stagnation Temperature: ~1,000 K 10,000 K
Total Enthalpy: ~1 20 MJ/kg
Gas Types: Air / Nitrogen / Helium (optional)

5. Operating Characteristics

Test Duration:

Shock / impulse: ~1 ms 50 ms
Arc-heated / quasi-steady: ~10 ms 500 ms

Operating Mode: Intermittent / Impulse

6. Heating Methods

Electric arc heating
Shock compression heating
Combustion or plasma heating systems

7. Key Components

High-energy driver section (arc heater / shock tube)
Settling chamber (high-temperature resistant)
Hypersonic nozzle (cooled, contoured)
Test section and diffuser
Vacuum tank / exhaust system

8. Measurement & Instrumentation

Heat flux and surface temperature sensors
Pressure and aerodynamic force measurement
High-speed optical diagnostics (Schlieren, spectroscopy)
Plasma and ionization measurement systems

9. Applications

Rocket and missile aerodynamics
Re-entry vehicle thermal protection systems (TPS)
Hypersonic vehicle development
High-temperature gas dynamics research
Ablation and material testing

10. Key Advantages

Realistic simulation of high-temperature flight conditions
Capability to study aerothermal and chemical effects
Supports extreme environment testing
Critical for next-generation aerospace systems

11. Customization Options

Higher enthalpy ranges (plasma/arc systems)
Extended test duration configurations
Specialized gas environments
Advanced diagnostic and optical systems

Positioning Tip

Place under:

Hypersonic Wind Tunnels High Enthalpy / Aerothermal Systems

This is a high-end research product, typically used by:

Space agencies
Defense laboratories
Advanced aerospace R&D centers

Advanced Testing Capabilities

The tunnel offers precise simulation conditions for hypersonic and high enthalpy flows, crucial for aerospace research and development. Customizable diameters and high operational temperatures enable material evaluation under real-world conditions, while optical and sensor-based measurement options ensure accurate data acquisition.

Sophisticated Control & Safety

A PLC-based automated system manages all tunnel functions, ensuring process reliability and quick operational start-up in under 90 minutes. Active water/glycol cooling and ceramic-coated surfaces safeguard against extreme temperatures, optimizing longevity and safety during prolonged usage.

Connectivity and Compliance

Licensed to international standards, the wind tunnel includes Ethernet, USB, and RS-485 data interfaces for seamless integration with laboratory setups and data networks. Its infrastructure aligns with ASTM and ISO protocols, delivering confidence and compatibility for global research teams.

FAQ's of Hypersonic High Enthalpy Wind Tunnel:

Q: How does the Hypersonic High Enthalpy Wind Tunnel benefit aerospace and material research?

A: This wind tunnel enables in-depth analysis of material and aerodynamic performance under extreme hypersonic conditions. Researchers can replicate real flight environments, test high-temperature materials, and analyze fluid dynamics, improving design accuracy and safety for advanced vehicles.

Q: What measurement systems are integrated within the tunnel for accurate data?

A: The tunnel comes equipped with optical windows for flow visualization, precision pressure sensors, and thermocouple arrays to monitor thermal and dynamic parameters throughout tests, delivering comprehensive and reliable data sets.

Q: When is the equipment ready for operation after installation?

A: Thanks to its automated PLC-based control system and streamlined start-up protocols, the wind tunnel can be brought online in less than 90 minutes after installation and setup, minimizing downtime for critical research projects.

Q: Where is this wind tunnel typically installed and used?

A: It is ideally installed in specialized research laboratories, aerospace research centers, and university facilities focusing on hypersonic aerodynamics and material science, where advanced experimental setups are required.

Q: What is the process for simulating high enthalpy and hypersonic flow conditions?

A: The process involves heating gases up to 5000 K using plasma arc technology, then accelerating them through customizable nozzles into the test section. The system monitors conditions and data in real time using its automated control and measurement modules.

Q: How can users access and manage experimental data from the system?

A: Users can retrieve and analyze experiment data via Ethernet, USB, or RS-485 interfaces, ensuring compatibility with standard data acquisition modules and laboratory networks for seamless integration and workflow efficiency.

Q: What are the main advantages of the tunnel's construction and safety features?

A: Manufactured from high-grade alloy steel with temperature-resistant ceramic coatings and active cooling systems, the tunnel ensures operational durability and safety even during demanding high-temperature runs, while maintaining noise levels below 80 dB(A).

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