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Aerodynamic Measurements of a Gulfstream Aircraft Model With and Without Noise Reduction Concepts
2014
20th AIAA/CEAS Aeroacoustics Conference
unpublished
Steady and unsteady aerodynamic measurements of a high-fidelity, semi-span 18% scale Gulfstream aircraft model are presented. The aerodynamic data were collected concurrently with acoustic measurements as part of a larger aeroacoustic study targeting airframe noise associated with main landing gear/flap components, gear-flap interaction noise, and the viability of related noise mitigation technologies. The aeroacoustic tests were conducted in the NASA Langley Research Center 14-by 22-Foot
doi:10.2514/6.2014-2477
fatcat:643v4r2vujdmvft636wmh7znsm