Towards Numerical Aircraft Noise Certification: Analysis of a Full-Scale Landing Gear in Fly-Over Configuration
Author:
Affiliation:
1. Exa GmbH
2. Gulfstream Aerospace Corporation
3. EXA Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2235
Reference24 articles.
1. Aerodynamics of a Gulfstream G550 Nose Landing Gear Model
2. A Comparative Study of a 1/4-Scale Gulfstream G550 Aircraft Nose Gear Model
3. A Hybrid Lattice-Boltzmann/FH-W Method to Predict Sources and Propagation of Landing Gear Noise
4. Preliminary Analysis of Acoustic Measurements from the NASA-Gulfstream Airframe Noise Flight Test
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