NASA Glenn Research Center houses a suite of specialized facilities dedicated to studying aircraft engine noise, with recent work focusing on measurement techniques and noise reduction strategies.
The 9- by 15-Foot Low Speed Wind Tunnel (9 x 15 LSWT) underwent modifications completed in 2019 to enhance flow control and reduce background noise. A newly installed five-sensor microphone rake enables precise capture of sound generated by scale experimental propulsors during testing of aircraft engine aerodynamics and acoustics under takeoff and landing conditions.
Housed within the Aero-Acoustic Propulsion Lab (AAPL), a 65-foot geodesic dome built in 1993, researchers conduct tests in an environment engineered to eliminate acoustic reflections. The dome incorporates 17,000 custom fiberglass wedges lining its interior surfaces to absorb sound, creating an anechoic or hemi-anechoic chamber. This setup supports three primary test rigs: the Nozzle Acoustic Test Rig (NATR), the Small Hot Jet Acoustic Rig (SHJAR), and the DGEN 380 Aeropropulsion Research Turbofan (DART).
SHJAR, one of three rigs within AAPL, specializes in testing single-stream nozzles up to 5 cm in diameter at Mach 2.0 and 800 K. It has served as a platform for developing advanced diagnostic methods, including Raman-based optical measurements for turbulent temperature fluctuations and digital Schlieren imaging. Three-dimensional microphone arrays deployed on SHJAR map noise sources, while time-resolved particle image velocimetry has previously captured turbulent velocity correlations in hot jets. These techniques contribute to validating computational models of jet noise, with findings informing nozzle design improvements.
NATR, a free-jet wind tunnel, enables evaluation of noise reduction concepts through scale model testing under simulated takeoff and landing conditions (up to Mach 0.35). Its configuration allows simultaneous far-field noise measurements across all angles, facilitating accurate translation of test results to real-world aircraft noise profiles. Over three decades, NATR has supported key developments, including the early testing of chevron nozzles that are now standard on commercial aircraft. The facility’s scale and integrated flow diagnostics and acoustics capabilities remain unique globally.
The DGEN 380, integrated into the DART test bed, facilitates experiments on turbofan noise, engine controls, and installation effects. Recent tests in August 2019 employed circumferential microphone arrays and sideline arrays to capture detailed acoustic data from nozzle exits, aiming to refine noise prediction methods and mitigation strategies.
The Acoustical Testing Laboratory (ATL), configured as an anechoic or hemi-anechoic chamber, supports diverse missions, including noise analysis for space station experiments and aircraft engine components. Its interior features dense rubber materials and 34-inch fiberglass wedges to absorb 99% of incident sound above 100 Hz. The ATL has been used to test supersonic inlet models and spacecraft ventilation systems, with ongoing research focused on reducing takeoff and landing noise through innovative engine placement.
NASA technical reports related to these facilities are accessible through the NASA Technical Reports Server (NTRS).

