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To learn more about the capabilities of the Aeroacoustic Propulsion Laboratory and to find out if it can be used for your test, please, contact:

James Bridges

+ Aeroacoustic Propulsion
   Laboratory

Testing Facilities
AERO-ACOUSTICS PROPULSION LABORATORY
PULSED DETONATION ENGINE

A pulsed detonation engine fires inside the Aero-Acoustic Propulsion Laboratory during acoustic performance tests.

Quiet enough to hear an engine
If you want to make aircraft engines quieter, sooner or later you have to listen to an engine. Ground tests of an engine give important information that can’t be obtained through scale model component tests or flight tests.

Was that core noise or was that fan noise? Does the noise reduction treatment we added need to be adjusted? These are the types of questions we have in mind when we run acoustic tests of engines in the AeroAcoustic Propulsion Lab.

The AeroAcoustic Propulsion Laboratory, (aka “The Dome”), has proven to be an ideal location for engine noise tests—from pulsed detonation subsystems to full fighter aircraft engines.

What makes the Dome unique? Topping the list is the ability to vent the hot engine exhaust through the large door of the Dome without using noisy flow collectors. And since anechoic wedges are installed on all surfaces inside the 65 foot radius geodesic Dome, far-field sound measurements aren’t contaminated by community noise or by reflections from lab equipment.

The AeroAcoustic Propulsion Lab has access to continuous flow compressed air at 100 psi, 150 psi, and 450 psi, as well as to compressed gas trailers (typically natural gas and hydrogen). Couple these services with the state-of-the-art instrumentation we have, and it is hard to imagine a better place to solve complicated engine noise problems.

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
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NASA Official: E. Brian Fite

Last Updated: July 8, 2008


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