X-59 CFD and Sonic Boom AssessmentsX-59 is a NASA experimental demonstrator aircraft designed to mitigate the adverse impact of sonic boom through advanced aircraft shaping methodologies. The Lockheed Martin (LM) Corporation was awarded a contract to manufacture the X-59 to demonstrate unique boom shaping technologies and address system integration challenges to be able to limit maximum sonic boom perceived level of loudness to be less than 75 dB across the entire carpet while cruising at a Mach number of 1.4. Initial flights and envelope expansion of the X-59 is expected to begin in 2022, with community tests expected at multiple locations starting from early 2024. This paper discusses the Computational Fluid Dynamics (CFD) analysis and sonic boom assessment of the X-59.
Document ID
20205003609
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
John M. Morgenstern (Lockheed Martin (United States) Bethesda, Maryland, United States)
Sriram K Rallabhandi (Langley Research Center Hampton, Virginia, United States)
Date Acquired
June 17, 2020
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: AIAA SciTech 2021
Location: Nashville, TN
Country: US
Start Date: January 11, 2021
End Date: January 15, 2021
Sponsors: American Institute of Aeronautics and Astronautics