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Development of a Trajectory-Centric CFD-RBD Framework for Advanced Multidisciplinary/Multiphysics SimulationThe desire to model increasingly complex unsteady flow phenomena drives coupling of physics-based disciplinary analysis tools, such as coupled aerodynamics-rigid body dynamics simulations. This paper documents the creation of a framework linking the six-degree-of-freedom trajectory propagator POST2 with NASA’s FUN3D computational fluid dynamics flow solver. Cross-code verification between the framework and a CFD-centric 6DOF code is performed using the Army-Navy Finner projectile experiencing unsteady accelerating flow. Free-flight simulations of an entry vehicle ballistic range test are validated against physical and computational experiments.
Document ID
20210024921
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Zachary J Ernst
(Georgia Institute of Technology Atlanta, Georgia, United States)
Madilyn K Drosendahl
(Georgia Institute of Technology Atlanta, Georgia, United States)
Bradford E Robertson
(Georgia Institute of Technology Atlanta, Georgia, United States)
Dimitri N Mavris
(Georgia Institute of Technology Atlanta, Georgia, United States)
Date Acquired
November 24, 2021
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: AIAA SciTech 2022
Location: San Diego, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80NSSC21M0050
CONTRACT_GRANT: NNL09AA00A
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
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