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Dynamic CFD Simulations of the Supersonic Inflatable Aerodynamic Decelerator (SIAD) Ballistic Range TestsDynamic CFD simulations of the SIAD ballistic test model were performed using US3D flow solver. Motivation for performing these simulations is for the purpose of validation and verification of the US3D flow solver as a viable computational tool for predicting dynamic coefficients.
Document ID
20160008070
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Brock, Joseph M (Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Stern, Eric (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
June 29, 2016
Publication Date
June 13, 2016
Subject Category
Astrodynamics
Report/Patent Number
ARC-E-DAA-TN33026
Report Number: ARC-E-DAA-TN33026
Meeting Information
Meeting: International Planetary Probe Workshop (IPPW 2016)
Location: Laurel, MD
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: Johns Hopkins Univ.
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Dynamic Stability

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