Aeroacoustic Computations of a Generic Low Boom Concept in Landing Configuration: Part 1 - Aerodynamic 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/10.2514/6.2021-2195
Reference28 articles.
1. Supersonic Technology Concept Aeroplanes for Environmental Studies
2. Khorrami, M.R. and Fares, E. "Toward noise certification during design: airframe noise simulations for full-scale, complete aircraft", CEAS Aeronaut J (2019) 10: 31. doi:10.1007/s13272-019-00378.
3. Simulations of a Full-Scale Aircraft with Installed Airframe Noise Reduction Technologies
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