DSMC-based correction factor for low-fidelity hypersonic aerodynamics of re-entering objects and space debris
Falchi, Alessandro and Minisci, Edmondo and Vasile, Massimiliano and Rastelli, Davide and Bellini, Niccolò (2017) DSMC-based correction factor for low-fidelity hypersonic aerodynamics of re-entering objects and space debris. In: 7th European Conference for Aeronautics and Space Sciences, 2017-07-03 - 2017-07-06.
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Abstract
This work investigates the differences between hypersonic aerodynamic coefficients computed with two different tools, having two different levels of fidelity: a high fidelity code implementing the Direct Simulation Monte Carlo method and a low fidelity one based on the approximated hypersonic local surface inclination technique. Different multivariate correction factors to reduce the low-fidelity tool error have been defined using a High Dimensional Model Representation algorithm. The low fidelity approach with the implemented correction factor has been tested on different space objects, the Gravity field and steadystate Ocean Circulation Explorer satellite and a 3U CubeSat with a deployed drag sail; the results are presented and commented.
ORCID iDs
Falchi, Alessandro ORCID: https://orcid.org/0000-0002-7452-5729, Minisci, Edmondo ORCID: https://orcid.org/0000-0001-9951-8528, Vasile, Massimiliano ORCID: https://orcid.org/0000-0001-8302-6465, Rastelli, Davide and Bellini, Niccolò;-
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Item type: Conference or Workshop Item(Paper) ID code: 61665 Dates: DateEvent3 July 2017Published31 March 2017AcceptedSubjects: Technology > Mechanical engineering and machinery Department: Faculty of Engineering > Mechanical and Aerospace Engineering
Technology and Innovation Centre > Advanced Engineering and Manufacturing
Strategic Research Themes > Ocean, Air and SpaceDepositing user: Pure Administrator Date deposited: 30 Aug 2017 09:08 Last modified: 14 Dec 2024 01:43 Related URLs: URI: https://strathprints.strath.ac.uk/id/eprint/61665