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A Database of CFD-Based Buffet Forcing Functions for Artemis I Structural Response EvaluationTime-accurate FUN3D simulations are utilized to estimate buffet-induced unsteady forces experienced by the Space Launch System during the Artemis I (AR01) flight. A set of FUN3D simulations was developed that employed time-accurate mesh translations to simulate the changing velocity and attitude based on the AR01 best estimated trajectory. In these simulations, referred to as accelerating-flow simulations, the freestream Mach number increased from 0.80 to 1.92. Additional time-accurate simulations were obtained at constant freestream Mach number equal to 0.95, 1.18, 1.70, thereby simulating stationary conditions experienced by the flow in a wind-tunnel. On the grounds of favorable comparisons between simulated and flight-measured environments, the FUN3D-based surface pressures were utilized to develop a buffet forcing function (BFF) database. This BFF database was analyzed to characterize the spatial distribution and frequency content of the buffet forces during transonic and supersonic portions of the AR01 flight. The region of interest is located downstream of the forward attachment (FA) hardware between the core stage and the solid rocket boosters where vortex shedding off the FA protuberance produces significant unsteadiness. The analysis reveals that, at transonic and supersonic conditions, buffet forces that are based on constant freestream Mach number data are a good approximation of those based on accelerating-flow simulations.
Document ID
20240014635
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Francesco Soranna
(Langley Research Center Hampton, Virginia, United States)
Craig L Streett
(Langley Research Center Hampton, United States)
Patrick S Heaney
(Langley Research Center Hampton, Virginia, United States)
Martin K Sekula
(Langley Research Center Hampton, Virginia, United States)
David J Piatak
(Langley Research Center Hampton, Virginia, United States)
Oleg O Goushcha
(Langley Research Center Hampton, United States)
James M Ramey
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
November 18, 2024
Subject Category
Aerodynamics
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 981271.02.40.04.03.50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FUN3D
structural loads
launch vehicles
transonic buffet
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