Modeling of Unsteady Aerodynamic Charactersitics of Delta Wings
2002 (English)In: Proceedings 23rd International Congress of Aeronautical Sciences (ICAS), Toronto: ICAS , 2002Conference paper (Refereed)
An analytic prediction model is presented to estimate aerodynamic coefficient of delta wing undergoing dynamic motions. The model is based on the introduction of a state space variable describing the vortex breakdown. This model will be suitable for modeling of flight dynamics in the preliminary design phase.
Place, publisher, year, edition, pages
Toronto: ICAS , 2002.
delta wings, unsteady, modeling, preliminary design, aerodynamic coefficient
Engineering and Technology
IdentifiersURN: urn:nbn:se:liu:diva-40989Local ID: 54823ISBN: 0-9533991-3-3 (cd-rom)OAI: oai:DiVA.org:liu-40989DiVA: diva2:261839
23nd Congress of International Council of the Aeronautical Sciences, Toronto, Canda, 2002 (ICAS 2002)