NASA Logo
+ NASA Homepage
+ About Us– Testing+ Analysis+ Collaboration+ Education+ Contact Us

Find Out More
To find out if Particle Image Velocimetry can be used for your test, contact:

James E. Bridges

Special Instrumentation
PARTICLE IMAGE VELOCIMETRY
Particle Image Velocimetry

Particle Image Velocimetry uses light reflected from seed particles in the flow to measure velocities of the air exhausting through nozzles.

Shedding light on the mysteries of high-speed hot jets
This we know—aircraft jet noise is caused by the intense turbulent mixing of hot high-speed exhaust gases and cool ambient air. By controlling the way a jet mixes with the surrounding air, we can potentially control the amount of noise it produces.

Easier said than done!

NASA Glenn is broadening our understanding of high energy flows through the development of advanced instrumentation systems like Particle Image Velocimetry (PIV). Systems like these allow us to gather new data that can be used to validate critical turbulence modeling quantities which are at the heart of many noise prediction schemes.

Particle Image Velocimetry is a technique used to measure unsteady velocities in hot jets. Particles are introduced to the stream(s) of interest which are illuminated by a sheet of laser light. Images captured by a pair of cross correlation cameras are processed, yielding turbulence data faster and in far more detail than previous techniques. More detailed measurements coupled with more accurate theories enable engineers to design quieter nozzles.

PIV is able to measure mean velocity, RMS velocity, and two-point correlation statistics which are all used to validate the latest aeroacoustic theories. And while there are a number of PIV systems are commercially available, researchers at NASA Glenn have recently deployed a new High Resolution Stereo Particle Imaging Velocimetry system that expanded the field of view to over four times that of the previous PIV system while dramatically reducing facility testing time and data acquisition system complexity.

PVI Thumbnail Watch real data in motion.
A new time-dependent PIV system developed at NASA Glenn was used to measure the unsteady velocities of the hot gas exhausting from a scale model of the dual-stream nozzle at takeoff conditions in the Aeroacoustic Propulsion Laboratory. A sheet of laser light illuminated a 13x75mm measurement region just downstream of the nozzle centerbody plug. It captured the action in the shear layer, an area of intense mixing where the inner core stream and the outer fan stream merge. This animation of actual test data shows how the velocities at 150 locations in the measurement region change in magnitude and direction over a 0.1 second interval (10 kHz sampling rate). The mean velocity has been subtracted from the data to highlight the unsteady flow.
+ View the animation
TESTING FACILITIES
+ Aero-Acoustic Propulsion Lab
+ Small Hot Jet Acoustic
   Test Rig

+ Nozzle Acoustic Test Rig
+ Advanced Noise Control
   Fan Rig

+ 9’x15’ Low Speed Wind Tunnel
+ Acoustical Testing Laboratory
SPECIAL INSTRUMENTATION
– Particle Image Velocimetry
+ Rotating Microphone Rake
+ Phased Array Microphones
+ Rotor Alone
+ Rayleigh Scattering
+ Hotwire, Hotfilm, and Laser    Doppler Velocimetry
Spacer
FirstGov - Your First Click to the US Government

+ NASA Privacy Statement, Disclaimer,
   and Accessibility Certification

+ Download Adobe Reader

Click to visit the NASA Homepage

NASA Official: E. Brian Fite
Last Updated: July 8, 2008


+ GRC Home