Aeroacoustic Computations of a Generic Low Boom Concept in Landing Configuration: Part 2 - Airframe Noise Simulations
Author:
Affiliation:
1. Dassault Group
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2196
Reference17 articles.
1. Supersonic Technology Concept Aeroplanes for Environmental Studies
2. Toward noise certification during design: airframe noise simulations for full-scale, complete aircraft
3. Simulations of a Full-Scale Aircraft with Installed Airframe Noise Reduction Technologies
4. Duda, B., Ferris, R. J., and Khorrami, M. R. "Simulation-Based Assessment of a Full-Scale Installed Quiet Landing Gear," AIAA Paper 2019-2476.
5. Comparison of Measured and Simulated Acoustic Signatures for a Full-Scale Aircraft with and without Airframe Noise Abatement
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