Creation of aerodynamic database for the X-31
2010 (English)In: 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2010, 2010-0501- p.Conference paper (Refereed)
Adaptive fidelity computional fluid dynamics (CFD) uses CFD tools spanning from vortexlattice methods codes to more advanced inviscid Euler solvers and finally URANS (Unsteady Reynolds Averaged Navier Stokes) CFD solvers. At the high end the automatization process is no longer a simple straight forward task, for this purpose a script-driven tool has been developed for integration into the multi-fidelity framework CEASIOM developed in the SimSAC project. The scripting technologies to prepare, conduct, post-process and collect aerodynamic forces & moments into the aero-dataset. The tool together with the CEASIOM framework has been applied to the X-31 to create an aerodynamic dataset that is then analyzed by the stability & control tool SDSA to assess the modes of motion inherent in the dataset.
Place, publisher, year, edition, pages
2010. 2010-0501- p.
Aerodynamic database, Aerodynamic forces, CFD solver, Control tools, Data sets, Euler solver, Modes of motion, Post process, Unsteady reynolds-averaged navier-stokes, Vortex lattice method, Aerodynamics, Aerospace engineering, Computational fluid dynamics, Aerodynamic stability
IdentifiersURN: urn:nbn:se:kth:diva-31397ScopusID: 2-s2.0-78649829466ISBN: 978-160086739-2OAI: oai:DiVA.org:kth-31397DiVA: diva2:403493
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition; Orlando, FL; United States; 4 January 2010 through 7 January 2010
QC 201103142011-03-142011-03-142014-08-29Bibliographically approved