Print Email Facebook Twitter Relaxed Static Stability Performance Assessment on Conventional and Unconventional Aircraft Configurations Title Relaxed Static Stability Performance Assessment on Conventional and Unconventional Aircraft Configurations Author Jansen, Q.J.M. Contributor Vos, R. (mentor) Faculty Aerospace Engineering Department Flight Performance and Propulsion Programme Flight Performance and Propulsion Date 2015-01-16 Abstract This thesis report researches the influence of a reduced stability margin on the aircraft performance of conventional and unconventional aircraft configurations. Unconventional configurations are defined as canard and three-surface aircraft. Subject Relaxed Static StabilityTail SizingUnconventionalStability MarginGround effect To reference this document use: http://resolver.tudelft.nl/uuid:d0450f45-f383-411e-b455-1eda6ace08e8 Part of collection Student theses Document type master thesis Rights (c) 2015 Jansen, Q.J.M. Files PDF MSc._Thesis_-_Quinten_Jansen.pdf 8.86 MB Close viewer /islandora/object/uuid:d0450f45-f383-411e-b455-1eda6ace08e8/datastream/OBJ/view