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Schlieren Systems

Individually crafted for supersonic wind tunnels and nozzle studies, transonic wind tunnels and more

Home > Products > High Speed > Schlieren Systems

AEROLAB’s Schlieren systems let you see shock waves as a combination of bright and dark areas.

In the study of supersonic flow, shock and expansion waves are used to determine Mach number. In most situations, however, they are virtually invisible to the naked eye. Fortunately, a system developed in 1864 by German Physicist August Toepler allows waves to be viewed clearly for accurate angular measurements.

Schlieren (plural for the German word “schliere”) are optical inhomogeneities in transparent materials. In supersonic flow, air experiences very large changes in density as it approaches, passes through and trails shock waves. As the density of air changes, so does its index of refraction.

Changes in index of refraction essentially turn the shock waves into lenses, bending the light. Toepler’s Schlieren “system” separates the light bent by the shock waves from the background light, allowing the shocks to be viewed as a combination of bright and dark areas.

AEROLAB offers individually crafted Schlieren Systems for any application: supersonic wind tunnels, transonic wind tunnels, supersonic nozzle study, etc.

Components

  • Light source – all-in-one solid state power supply and short-arc xenon lamp with lens, track-mounted adjustable aperature (100-250 VAC 50/60 Hz)
  • Two telescope-quality parabolic mirrors – frame mounted with fine adjustment knobs
  • Knife edge – adjustable in all three axis and angle of inclination with fine adjustment knobs
  • Plain mirror – first-surface to reflect the image to a convenient viewing location
  • Viewing screen

Standard Mirror Sizes

  • 6-inch mirrors and 48-inch focal length
  • 8-inch mirrors and 64-inch focal length
  • 10-inch mirrors and 80-inch focal length
  • 12.5-inch mirrors and 100-inch focal length

Optional Features

  • Custom Sizes

Related Products

  • Supersonic Wind Tunnel
  • Transonic Wind Tunnel

Type

  • High Speed

Components

  • Light source - all-in-one solid state power supply and short-arc xenon lamp with lens, track-mounted adjustable aperature (100-250 VAC 50/60 Hz)
  • Two telescope-quality parabolic mirrors - frame mounted with fine adjustment knobs
  • Knife edge - adjustable in all three axis and angle of inclination with fine adjustment knobs
  • Plain mirror - first-surface to reflect the image to a convenient viewing location
  • Viewing screen

See the Schlieren Systems brochure

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Navigation
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    • History
    • Leadership
  • Services
    • Design & Analysis
    • Fabrication
    • Installation
  • Products
    • Subsonic Wind Tunnels
      • Open Circuit Wind Tunnels
      • Closed Circuit Wind Tunnels
      • Educational Wind Tunnel (EWT)
    • Low Speed
      • Blow Down Wind Tunnels
      • Closed Circuit Wind Tunnels
      • Educational Wind Tunnel (EWT)
      • Educational Wind Tunnel Upgrade
      • Open Circuit Wind Tunnels
      • Wind Generators
    • High Speed
      • Schlieren Systems
      • SuperSonic Wind Tunnels
      • Transonic Wind Tunnels
    • Balances
      • Pyramidal Balance
      • Sting Balance
    • Low Speed Models & Probes
      • Clark Y-14 Slat/Flap Wing
      • Drag Model Set
      • Flat Plate and Mouse
      • Pitot-Static probe
      • Pressure Cylinder
      • Pressure Wing
      • Scaled F-16/Custom Aircraft Models
      • Turbulence Sphere
      • Wake Rake
      • Wind Tunnel Test Models
    • High Speed Models & Probes
      • AGARD-B
      • Cone
      • Force Missile
      • Pressure Missile Model
      • Sphere
      • Total Pressure Probe
      • Wedge
    • Specialty Tunnels/Equipment
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      • Model Positioning System
      • Traverse Systems
      • Water Tunnels & Channels
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