High Speed Jet Facility

Equipment Specifications : High speed compressor with separate tank, coflowing jet,
Equipment Application : Experiments on jets and Nozzles
Technical Specification : 18HP 3-phase triple cylinder motor, 8000litre tank

Description

A High-Speed Jet Facility is a specialized experimental setup used to study supersonic or hypersonic jet flows, typically in the fields of aerospace, fluid dynamics, combustion, propulsion, and acoustics. These facilities are designed to simulate high-velocity gas jets under controlled conditions, enabling research into complex flow phenomena.


???? Key Purposes

  1. Study of Supersonic & Hypersonic Jets

    • Mach numbers typically ranging from 1.5 to 5+.

    • Relevant to rocket nozzles, jet engines, and re-entry vehicles.

  2. Aeroacoustics Research

    • Understanding noise generation mechanisms in high-speed jets.

    • Supports development of noise reduction techniques.

  3. Combustion & Propulsion Testing

    • Investigates fuel mixing, ignition, and flame stability in jet engines.

  4. Shock and Flow Structure Analysis

    • Visualization and measurement of shock waves, turbulent mixing, and shear layers.


???? Core Components of a High-Speed Jet Facility

Component Description
High-Pressure Gas Supply Provides compressed air, nitrogen, or combustion gases at pressures typically 5–100+ bar.
Nozzle Convergent-divergent (C-D) nozzle to achieve desired Mach numbers. Can be interchangeable.
Test Chamber / Jet Test Section Enclosed or open area where the jet is released into ambient or vacuum conditions.
Heater / Combustion Unit (Optional) To simulate high-enthalpy or hot gas jets (e.g., in rocket exhaust).
Instrumentation Includes pressure transducers, thermocouples, Pitot probes, etc., for measuring flow properties.
High-Speed Schlieren / Shadowgraph System For visualizing density gradients, shocks, and turbulence.
Acoustic Measurement System Microphone arrays and data acquisition systems to study jet noise.
Data Acquisition & Control High-speed systems to record time-resolved data and control facility parameters.

???? Key Parameters Typically Investigated

  • Mach number (M): 1.5 to 5+

  • Stagnation pressure and temperature

  • Jet velocity and turbulence characteristics

  • Shock cell structure and spacing

  • Jet mixing and plume spreading

  • Far-field and near-field noise

  • Jet impingement effects (if applicable)

Reviews

There are no reviews yet.

Be the first to review “High Speed Jet Facility”

Your email address will not be published. Required fields are marked *