Print Email Facebook Twitter Semi-Analytical Composite Oval Fuselage Weight Estimation Title Semi-Analytical Composite Oval Fuselage Weight Estimation Author Roelofs, M.N. (TU Delft Flight Performance and Propulsion) Vos, Roelof (TU Delft Flight Performance and Propulsion) Date 2017 Abstract To reference this document use: http://resolver.tudelft.nl/uuid:c9e2a32f-5e0d-4b4d-acba-0a5e04402cb3 DOI https://doi.org/10.2514/6.2017-0466 Publisher American Institute of Aeronautics and Astronautics Inc. (AIAA) Embargo date 2018-01-06 ISBN 978-1-62410-447-3 Source 55th AIAA Aerospace Sciences Meeting: Grapevine, Texas Event 55th AIAA Aerospace Sciences Meeting, 2017-01-09 → 2017-01-13, Grapevine, United States Part of collection Institutional Repository Document type conference paper Rights © 2017 M.N. Roelofs, Roelof Vos Files PDF journalstemp.pdf 2.99 MB Close viewer /islandora/object/uuid:c9e2a32f-5e0d-4b4d-acba-0a5e04402cb3/datastream/OBJ/view